Some corrections: Thanks to @slome815 for pointing out there was one other launch system with no escape provision: Voskhod. I completely forgot about that one. I said FBW was ‘the norm’ in 1968. That’s not correct. Irreversible controls were but fbw was in its infancy. There is a correction to kind of address it at 49 minutes and I’ll be doing an entire video about it in a few weeks. Thanks @SoloRenegade
A future system also lacking a LES is the SpaceX Starship, though that project has such an array of fundamental issues facing It that I doubt that it will even fly freight to orbit.
@@Miata822 I've made the decision to only do videos on things that already exist (ie not CGI renders or half baked tests). If Spacex put humans in anything that even remotely resembles their starship proposals, I'll go there.
Gemini also didn't really have an escape system. Sure, they nominally had ejection seats, but a) Those would only be good for the first 40 seconds of launch, after that the spacecraft would be going too fast for the ejection seats that were fitted to be reliable, and b) I really do not like the prospects of firing an ejection seat charge inside a spacecraft that is pressurised to 1 atm with pure oxygen and has been soaking in that pure oxygen for over an hour prior to launch.
@@zuthalsoraniz6764 That's part of the design. The flash fire in the cabin as ejection motors fire helps precondition the astronauts and seats for the presumptive fireball they are ejecting into. /jk
One of the Mercury/Redstone engineers is still with us. He is 92 years old and comes to our shop for little machining jobs he can’t do in his home shop. Talked to him about meeting Wehrner Von Braun down in Alabama. He described the man as a skilled publicist and salesman as much as he was a scientist and engineer. Old Lyle is living history. Every time I see him is a bonus.
A Nazi is a Nazi but Von Braun was exceptional. He killed more people assembling his V-2 than did the business end of it. By the gods that is what it is about wasn't it, the eradication of the Jews. How soon we forget what the man did just so we could get to space. NEVER FORGET! It is another sin this country has to endure that we didn't punish him and his countrymen, the greedy lot we are.
I was volunteering at a space museum this weekend alongside a 96 year old data reduction specialist who worked on the Snark program. He did a bit of work with computers to extract data for Von Braun when he was having trouble getting data in a timely fashion at Cape Canaveral, but only with the consent of Jack Northrop since that's who he really worked for (!). Fascinating, fascinating guy, really glad I got to spend some time with him this weekend.
My Uncle used to be one of Werner Von Braun's pilots when he was based in Alabama. (IOW, he flew one of the planes that Von Braun used to get around the country)
Years of testing separate Virgin Galactic from Oceangate. If Titan tested as hard as Spaceship Two it would have imploded years before it started carrying passengers
There is one major difference: One of them knew what he was doing despite taking very weird and somewhat unsafe approach. Other was a rich idiot. One is alive, other is red mush.
@@banksuvladimirit's one guy and one company, but one exception is enough to disprove the rule of "but the pilots wouldn't be in it if it weren't safe"
With respect to the "pilots wouldn't do it if it wasn't safe": I know one of the astronauts who was on the return to flight mission after the Columbia shuttle disaster. He told me that the pilots and most of the astronauts (at least) would have gone up in a shuttle the next day if they had been allowed to. They are probably more capable of understanding the risks of spaceflight than most people. They would have been willing to take the flight before anyone really even understood what happened. I would be willing to count that as "informed consent" but it had nothing to do with whether they believed it was safe (to the extent that spaceflight can be safe.) They understood the risks as well as anyone and decided it was worth it. Many people would do these things despite them being unsafe, and that's fine, but for a layman to have informed consent, the risk needs to be appropriately characterized.
True. To make a car compassion. I don't think any enthusiast wouldn't want to drive a F1 cat. Problem is 95% wouldn't even be able to press the brake pedal hard enough to stop fast enough when actually going fast.
"I had been conditioned to believe that there is nothing more dangerous than the arrogance of ignorance; now I would learn that it does not compare with the arrogance of knowledge, knowledge that is often confused with wisdom." -John Piña Craven, 1959, on being appointed Chief Scientist of the US Navy.
That's the same period of time that John Clark (author of _Ignition!_ (1972), a great technical autobiography of rocket fuel development) was running the rocket fuel lab at the US Naval Air Rocket Test Station (NARTS) for 17 years while avoiding any time-lost accidents. From some of the stories he tells, it was by careful understanding and caution when pushing near any sort of limit, whether knowledge or operation.
Military systems engineer here. "Procedure" is *literally* the second to last choice for risk mitigation (the last choice being a placard, i.e., "YOLO - here's a sign to tell you to watch out for that!").
Depends on kind of person you're designing it for. I remember seeing something to the effect of "don't weld with ammunition present" on an ammo box on a US WW2 era warship.
@@sruz25cz This is what makes safety engineering in military systems so interesting to me as a civilian layperson. You can do all the traditional risk mitigation that you want, but to have an effective military you absolutely will need to put people with a wide range of backgrounds, education, and life experience directly in the path of some pretty dangerous situations even in peacetime. Finding where to draw the "we've done all that we can" line under such circumstances must be quite challenging, with some serious repercussions if you get it wrong.
@@sketchyAnalogies I've always wondered about this hierarchy. Whether administrative or PPE are less effective controls depends a lot on context. For instance, shoes are a form of PPE, but they're a much more effective control against foot cuts than a sign saying "sweep up all sharp objects". But administrative controls are definitely more effective in high risk cases. For instance, arc flash suits and ejection seats are absolutely the last line of defense.
The mirage III had hydraulic controls, but the stick was linked to mini-control surfaces in the middle of the delta wing giving back-force to the pilot
For all the bigger jets back in the day the AMM/IPC was all on microfiche for that reason; I've seen a full 747 AMM and it was something like I think 12 or 13 binders, each SUPER thick, like 6" thick. Literally 2 binders just for all the wiring diagrams
As someone with a passion for engineering this is the kind of content i crave. its a refreshing break from alot of the content out there that basically just reads off the wikipedia page. also as a sidenote, ive also designed my own hybrid rockets and have recently been working on one basically the same as yours but i couldnt think of a decent way to break the nitrous cannister so thanks for that 😅
Ha! There are way better designs that use a meltable plastic disc and seals: you screw the canister down onto a spike to puncture it and it seals until the igniter melts the disk. I didn't bother with all that but I may in a future design.
My trust of transport platforms is now is based on the probability of an incident being followed up with the global engineering community collectively asking "well what did they expect?"
Part of my day job involves compiling reports with data from engineers on failure probabilities. The numbers show certain things to be highly improbably ... until they occur. When calculating how many sides on the die, there is never enough information to really nail it down. Hundreds or thousands of hours of analysis sometimes is no better than a WAG. In my world, even a tiny chance of something going wrong in a given hour gets multiplied by tens of millions of hours.
This is something I have to explain often in my job too: 'yes there's a one in a million chance, but we're going to run this 10 million times so it'll probably go wrong'. Communicating this kind of risk can be really really difficult.
@@jackee-is-silent2938 Just when you think you've got all of the failure modes covered, the real world finds more. But there is literally a practical limit to testing; our last jet engine certification cost more than two billion dollars before a single product hit the market.
@@jackee-is-silent2938 and be so ungodly expensive that you'll never sell it. good intentions never work like you want. stop living in fear of death. stop being a bubble boy.
When I was in Space Camp I asked what would happen if the explosive bolts didn't fire when the SRBs were ignited. The engineer who was talking to us just shrugged and went "The boosters tear them off and you launch anyway."
I always like to ponder what’d happen if the bolts only fired on one side. Obviously, hypothetical only since there were wired up in such a way to make that basically impossible. But fair to say the result would be…..a mess.
@@Alexander-the-okit would be a mess for sure, but that's the deal with solid rocket boosters. It's why I am always hesitant when it comes to grading safety on anything that relies on them. If you encounter an issue during throttling up of a liquid engine you can shut it down. You can scrub the launch, or in the case of an in flight problem, you can fall back on any number of your other engines to pick up the slack. You can't so that with an SRB. As soon as those light up, you are going to space, no matter if you want it or not, or if it will be in one piece.
@@mobiuscoreindustries The available evidence indicates SRB ignition can result in an apogee as low as 20 km. I wouldn't call that "going to space" when weather balloons regularly exceed 30 km altitude.
@@CoastalSphinx This is a way of saying. You cannot turn off the boosters, once they are ignited you have no other choice but to launch, otherwise you will likely cause a catastrophic failure on the launch pad. The boosters alone will not carry the vehicle to orbit of course but they are responsible for a large part of the thrust. Now with a LES the crew may get out safely but its suboptimal for the infrastructure to be kinda forced to launch a rocket you know to be deffective because holding onto it would be so much worse
Hello, loved the vid just popping in as a colourblind person to say I can't tell the difference between the yellow and green used in the Venn diagram. I get that it fits our established associations with the colours, but adding some sort of pattern marker would be huge in the future. Horizontal, vertical, diagonal, stripes or dots or something like that.
Oh man sorry about that! I had comments on earlier videos about font color but didnt think about it for the venn diagram. I’ll follow an accessibility guideline next time.
I think Alexander already gets this, but it's worth pointing out: The presence of an LES isn't important, what matters is how many failures and at what point in the mission will result in survival vs. death. If you focus more on the presence of a system than its capabilities, you can end up thinking ejection seats are a good idea in vertically-launched, vertically-landing spacecraft, for example. A proper escape system will be good, but it needs to actually be an effective design.
@@alexturnbackthearmy1907 I'd argue that they are a bad idea if it's vertically launched and vertically landing for a combination of factors 1. If it's vertically launched, astronauts will be on their backs, so they aren't going to gain altitude from ejecting. You can fix this with a big net, but it becomes more and more questionable that this is cheaper than a proper LES 2. Pressure suits don't provide protection against rocket exhaust or high-speed air. For example, the Space Shuttle is moving too fast for safe ejection after just 100 seconds 3. They add a bunch more things that can go wrong. Take that flight where the hatch blew off by accident on landing. If you need the ability to eject, the hatch needs to be fitted something like that, plus of course the rocket motors in each seat, which would have killed the other crew pretty quickly back when capsules used pure oxygen 4. Given the added weight and added complexity, I have my doubts that they are even all that much cheaper than a standard, tower-based LES, while offering much more limited capabilities and more failure points.
What a superb feature: using well-researched and referenced information to build a compelling argument. It’s quite accessible, yet detailed. You’ve found a new subscriber.
Really enjoying these deep dives. Thank you for the work you put in on this. "I do not care if operators are sued or not, this conversation is about safety." Lordy if I didn't end up walking away from a health and safety position when I realized all I was supposed to do was minimize liability. God forbid we actually make things safe.
Thanks. Yeah…..for better or worse, financial liability can be an incentive for good safety practices. But it’s really depressing to see much of the discourse after an incident being ‘I hope X gets sued’.
This is about science not some morbid false ideology in a non existent, non proven, sky daddy. Religion and schizophrenia go hand in hand. Seek psychiatric help.
I liked my university's risk management department back when we were doing rocketry. We found a way for the liability and the safety to align, such that the university is happy, the safety people are happy, and we are safe and doing cool things. Workplace safety, though? I have to essentially remind them that this email will look really bad in a lawsuit in order to get them to reorder PPE.
I too, have always had concerns, when I've heard the statement "it must be safe otherwise the pilot wouldn't fly in it" as history books are full of stories about dead pilots. I do, however, believe there's a 99.9999% chance the pilot will do as much as humanly possible to avoid disaster. Germanwings flight 9525 is one of the reasons it's not 100%.
If anybody ever says, “the pilot wouldn’t fly it if it wasn’t safe,” remember Eric Brown, who was a good pilot, BUT insisted on flying the ME163, despite warnings from the German ground crew.
Great video! Have always found the Rutan/Virgin Galactic model/approach a bit sketch... Minor quibble, at 49:29, that's not Charlie Brown, that's Linus Van Pelt!
For what its worth, Virgin fired their chief test pilot because he reported an almost fatal incident during one of their test flights to a reporter at Washington post. Essentially, acting as a whistle blower. The RH horizontal stabilizer exploded during boost. About 40 seconds in if I remember correctly. Anyways... their main oxidizer tank is growing weaker and weaker...
I took the footage used in your opening. There are some gaps and anomalies in the publicly available data about the 2014 crash. It is possible that something happened before the feather mechanism was activated, something that Alsbury was responding to. Nitrous can act as a monopropellant with a very energetic decomposition. If this happened inside the fuel injector valve it would have weakened the structure in a way that is consistent with the geometry of the breakup and with long range photography of the mishap.
I work on liquid rocket motors and as i've heard a colleague of mine who worked on a previous hybrid rocket motor say- Solid rockets don't want to shut off, liquid rockets don't want to start, and solid rockets don't want to do either
@@RENO_K The third phase should be "Hybrids don't want to do either." A hybrid's solid grain is difficult to light because you have to spray oxidizer across a large area and get that area ignited, needing a large, energetic pyrotechnic- a significant solid rocket motor in itself. Then when you cut off the oxidizer (either by running out or closing the ox valve) you have a large area of hot fuel grain that continues to evolve gas for a long time. On the other hand, with a small liquid motor, I've tapped out Morse code just because I could :)
Civil engineer.. Love the video. I know you're specifically talking Virgin Galactic but overall a brilliant presentation that well summarizes the state of "safety" in the billionaire unknown-tourism industry (space/ocean/etc). I hope against hope we see more change towards understanding this way of thinking without more accidents happening first.
My degree is in civil engineering too actually. My main concern is this 'free market will solve safety' ethos creeping into everyone's lives - willing participants or not.
@@Alexander-the-ok If the safety failures are fear-inducing enough, they aren't wrong -- the free market will solve safety -- just look at commercial airlines. It's hard to imagine the NTSB being formed and the FAA being held to account without the profoundly fear-inducing media coverage of airline crashes. Sure, the safety improvements rely upon unwilling participants dying but over 100 years they did seriously improve the safety record. Road traffic, on the other hand, is terrifying only if you understand statistics and safety factors. (I still get very anxious standing on street corners waiting to cross at busy intersections with vehicles traveling at 40 to 50mph, very high alert -- and predictable "accidents" every few months)
@@stephenkalatucka6213 Even from that point of view plenty of common/poor people get caught up in disasters like the Titanic. If people volunteer themselves for Darwin Awards that is definitely their freedom.
The Apollo Computer F-8 sounds like an interesting story, but what I want to hear about even more is the MR-1 launch (or just mercury-redstone in general)
The F-8 digital fly by wire is fast becoming my favourite for next video. I may do MR-1 in a ‘Christmas special’ of comical failures or something daft like that.
It was because of two cables separating in the wrong order. Because of this, significant power went through a relay which tripped a command since the control cable was supposed to separate first. The command was meant to separate the abort tower AND the booster from the capsule. To prevent the capsule from separating from an accelerating booster, the booster separation could only occur when the spacecraft was in ~0 g. Since it was on the ground, the sensors showed a booster accelerating by 1g constantly, so the abort tower was the only thing that jettisoned. That's not all, though. The recovery parachutes also activated since the capsule was detected to be under 3 kilometers and so it thought it needed to deploy the parachutes. Since the recovery system detected no load on the parachute since the capsule wasn't falling, it deployed the reserve parachute as well. The capsule was undamaged and was reused for MR-1A, and the missile was sent back to huntsville for refurbishment and a potential flight in future, but was eventually placed on display.
The amount I learned from this video about laws, planes, spacecraft, flight control systems, regulations, ethics, rocket engines, aerodynamics, systems design, automation and insomnia are exceptionally impressive. Thank you for this wonderful presentation and previous presentations on submersibles along with the associated sources, plenty of things to dig into. I really look forward to future videos.
"This video is not a billionaire showdown" thank you so much for this haha it's getting really tiring to always hear about the billionaires who own the company when people report on space news
You don’t have a ton of subscribers yet. But your content reminds me of Perun, the defense economics UA-camr who blew up since the full scale invasion of Ukraine. I’m looking forward to when you do your 100k subs video and I can say I was there before 10k ❤
I literally had the thought watching perun of “damn this is good, but I wish I could get this for non defense engineering”, found your channel the same day. (:
Calling them Astronauts and Mission Specialists is for the same reason they were Mission Specialists on the Titan. The informed consent rules are certainly different for "Crew" compared to "Passengers". The liability laws probably parse depending on if it is a 'customer' vs 'crew'. They are not calling them that just for marketing.
Except that entire statement is nonsense. The informed consent rules in this case are literally laws and regulations enforced by the FAA. They are literally just calling them that for marketing. SpaceShip2 is certified for human flight with passengers by the FAA.
Perhaps the FAA has not demanded certification for Virgin Galactic nor Blue Origin because they are not in the business of *transportation*. Their sub-orbital craft are essentially glorified amusement park rides.
Right now the FAA doesn't actually have authority to crew rate space vehicles, they apply the same rules to crewed and uncrewed launch vehicles (those requirements are higher than NASA's requirements for uncrewed but lower than their crew rating). NASA and the DoD both require and perform crew rating if you're working with them, but Virgin Orbit is isolated from Virgin Galactic so that doesn't apply here. New Shepard is in a gray area since Blue Origin does do business with both, but has not flown crew for either. New Shepard is technically crew rated, having done all the tests required and meeting the requirements in principle (like having no abort black zones) but I don't think that NASA actually audited that testing because they've only shown interest in uncrewed launches for scientific instruments.
Excellent presentation! With how few incidents there have been there's not much info or discussion of safety in space tourism. I think there will need to be more refinement of designs and procedures as it gets more mainstream with a larger customer base. Unlike air travel or extreme tourism "experiences" though it presents many unique challenges and may never reach the same level of safety.
That’s what drove me to making this video. There is virtually no critical analysis of VG. Almost everything I can find is blind optimism, nonsense about their stock price or advertising.
"informed consent", by design, requires information to make a consensual judgement. Commercial secrets kinda sort of make this a bit tricky. One would have to be a bit of a nutter to go up in the thing, hey.
My very over-simplified solution would be ‘to be covered by informed consent you are required to open-source your design’. Its problematic but a start. Companies that are allowed to operate without liability are essentially getting a free lunch.
You don’t need to be nutty, just misinformed. Most people, including me, don’t have the capability to do proper risk-analysis, let alone risk-analysis that takes to account gaps in knowledge or information. It’s also worth stopping and considering how ridiculous knowledge over wide range of fields one would need to have to give informed consent to space flight. Being able to consent without being properly informed means trusting some party based on reputation alone: and in this case the trusted party is the other side of the agreement…
@@catcatcatcatcatcatcatcatcatcaWhich is why it should be subject to certification process, meaning that a completely independent team of experts has assessed the risk.
Or you could all stop whining and realize that shit like this will happen when pushing boundaries in extremes. It’s absurd that you people want to grind the works to a halt over someone who chose to do a dangerous job dying. Faceless nobody blue collar workers die all of the time to keep things up and running and keep you air conditioned and comfortable. But when need to be forever bogged down in a ridiculous quagmire to try to prevent anyone from ever getting a boo boo while going to space
@@Alexander-the-ok several CPU design teams would no doubt agree and probably go up. On the other hand, several cryptography implementation teams would probably agree and still not go up in an open source space ship hehe
From calculations and engineering done later, I think that the space shuttle having about 65 sides is optimistic, as many avenues of failure did not result in disaster due to a massive amount of luck.
The early space shuttle missions were later estimated to be between 1 in 9 to 1 in 25, but later missions with safety improvements put that up towards 1 in 100. The NASA commercial crew program aims for a minimum failure rate of 1 in 300. That might be good enough for 4 flights per year to the ISS, one disaster in a lifetime, but I don't think that's what we are wanting if we are talking about space tourism. And I think Virgin might be around 1 in 20 right now, maybe 1 in 100.
The problem is that NASA failure estimates had absolutely no scientific validity. The numbers were just pulled out of their asses. That's why the program was ended. It was a boondoggle from the beginning, with no conception of how it was ever going to meet its stated objectives.@@phillyphakename1255
"I wish her and the other passengers the best of luck, though I do not know how much they will need." Absolutely excellent closing statement! Really drives home how little is disclosed by the company regarding safety systems.
I appreciate your professional approach to presentation of content - specifically, clear LIMITATIONS and disambiguization of "conflict of interest or endorsement" Your structure adds to ease of understanding concepts. Keep up the great work!!
Mike Adam's accident was due to him experiencing vertigo and positioning the aircraft essentially perpendicular to its flight path while at high altitude... Hard to picture! Shortly after, while re-entering the denser atmosphere, the aircraft entered a spin as a consequence. The initial trigger was, as far as I remember, some kind of electrical failure that distracted him. But vertigo was the overriding factor. It was learnt after the accident that he had been prone to it during his initial flight on the X15.
I disagree. I led development on SS1 hybrid motor. Just from watching videos on UA-cam I believe it suffered some sort of valve anomaly. I had seen that type of anomaly phenomena before. Failure modes can vary. The end result is clearly much lower thrust. It’s clear to me that the video shows ignition was normal. Black smoke as the solid rocket motor starts the hybrid looks ok. The initial start looks normal. What follows is more serious. Videos make it clear that the rocket was never shut off successfully. I wish I could see the motor chamber pressure when Mike Asbury unlocked the pneumatic feather booms. The feather mode has saved the spaceship a few times at much slower speeds. It’s possible the crew saw increased nitrous pressure in the tank due to a valve fire. If Teflon seals were used, anything is possible depending on the design. From the video, it looks like the Nitrous is decomposing and burning something other than HTPB. Just a guess. I think the answer lies in the fluid flow system and the motor chamber pressure when the boom was unlocked as a way to slow the vehicle down and start dumping the nitrous. The vehicle was not designed to land with the full tank of nitrous. On SS1, I required the nitrous dump valve requirement to empty the tank in an emergency is under 2 minutes. The nitrous load full was 3000 lbs. Note: I was not an employee of Scaled after SS1 went to Smithsoneon.
It is only a matter of time until there is a space tourism accident on par with what happened with the OceanGate Titan, and then people will start asking questions about the safety standards or lack thereof in the growing private space industry.
Just because Branson flew in Spaceship 2 doesn't mean Virgin Galactic has done adequate safety assessments internally. Rush chose to dive his Titan under similar conditions, and died in it. It should also be noted that Starship doesn't currently have a planned crew escape system in its design, though that might change in the future.
Starship does not have a planned Launch Escape System but they also don’t plan to fly any humans on it before the number of uncrewed flights has reached into the hundreds. This buys down a lot of the risk.
@@TheMcspreader Starship could escape SuperHeavy only in very specific scenarios where they can throttle down most of SH’s engines. Otherwise it’s thrust to weight ratio is far far too low to out accelerate SuperHeavy. Also it can’t escape from itself and it’s far more dangerous itself than a capsule that only has a minimal number of engines.
@@Borodalf Correct. Starship's thrust-to-weight would have to astronomically improve to, say, escape a Challenger-type scenario. Being on the front of Super Heavy instead of hanging off the side isn't enough. Perhaps some extra internal SRBs on crew-rated Starships? Maybe even an ejectable crew section. Unfortunately, in the current design I don't see anyway not to at least take the header tanks with the crew section...
43:00 If the aircraft is actively nosing up to bleed velocity and extend range, that isnt a ballistic reentry. Ballistic is a reference to the parabolic path of travel (though, this of course is shortened by the atmosphere as seen with true ballistic reentries with Soyuz craft). If I'm not mistaken, the Apollo capsules technically weren't ballistic entries either due to the heat shield acting as a lifting body due to the angle of attack. Great video, though!
1. They *have* a real VP of Safety? 2. Based on my private sector experience, no way in hell would I want to be responsible for safety at a private space company. The profit lust compromises everything, the need to please investors leads to pressure to overpromise and then cut corners trying to fulfill those overpromises.
Presumably you start in the job because it's a noble thing to try and keep the profit chasers in check. Then once you find out they can't be held back, you feel you daren't leave because of what you fear they might do if you weren't there.
At 32:15 - my guess is that passengers are referred to as “Astronauts” as part of a bid to avoid legal repercussions in case of a fatal accident á la the Oceangate titan implosion
I doubt it - I think it has more to do with ego stroking of the very wealthy who pay to ride. "Well if the company called me an astronaut, I must really be one!"
The reliance on "good pilots" as a security blanket has and will ever continue to cost lives, as has trusting the opinion of esteemed individuals such as Rutan without adequate risk assessment. Look at Apollo 1. After nearly drowning in the Liberty Bell 7 when the door inexplicably blew out on splashdown, I've read that the use of an inward-opening plug door on the Apollo capsule was one of Gus Grissom's (and other Apollo 1 astronauts') many demanded specifications for the crew module. And nobody was willing or able to convince him otherwise. It was going to be his craft to command and he was a national hero with unquestionably qualifying experience and credentials. He was truly a guy with "the right stuff" who had been there and done that in an era when almost nobody else had. But then came the plugs-out test and the fire and the door couldn't be pushed in or blown out. And Harrison Storms at North American Aviation was scapegoated for it, because who would even hint at a dead hero sharing any of the blame for his own death? Or that's how I read it. It's not like I was there. I've also read the astronauts suggested an outward opening hatch, which would conveniently absolve them of any blame, despite the inward opening hatch being included in Gemini craft. Not sure we'll ever know the truth.
Hybrid motors have a horrible tendency to spall off chunks of fuel that can get wedged in the nozzle causing a massive thrust asymmetry or worse over-pressure of the motor casing.
13:25 - There has been one (or two) more suborbital crewed space flight not in your list. Notably, it was an *attempt* at orbital space flight, though. Soyuz 18a had an in-flight launch anomaly that caused the flight to be aborted (the third rocket stage lit its engines while still being attached to the second stage, so the Soyuz capsule engines fired to pull it away from way-off-target launch vehicle.) This capsule reached a height of nearly 200 km, more than high enough to be “a space flight.” Although if we’re counting Virgin Galactic, then another in-flight-abort should be counted, too. Soyuz MS-10 experienced a similar launch booster failure, which caused it to separate. It reached 92 km of altitude, high enough for the 80km definition. There was a third Soyuz crewed abort, but it was on the pad, so reached nowhere near space.
Amazing video. I have always been mystified by the lack of good info on these crafts, but just wrote it up to me not being too much of a space or aviation nerd to know where to look. But this explains so much.
When people use the "pilots do it" argument, they miss a very important point, those pilots are not average people they are test pilots, with who knows how many hours of experience and a death wish. Let's differentiate that any risk has two independent factors, the inherent risk and the "if you stupid" risk. There are many people doing dangerous work, but as long as you stick to the rules you're very likely will be fine, but than again, there are special cases when you have both inherent and stupidity risk and need the truly unhinged who would happily sacrifice their own life just to help humanity progress a little bit. Those scientist come to mind, who designed the ejection seat, and tested the human tolerance for G force. Hats off to people like that.
Informed consent is a funny concept. In the last few years commercial tandem BASE jumping started popping up. None of the clients would do it if they had a clear view of the list of things that can go wrong. People just read "danger: death" and brush it off like they would read it in their car user manual.
In some sense, in specific areas of life, participation in democratic governance is the only form of agency individuals could ever have. Private companies are at the mercy of each other, as the competition might reward strategies majority of the individuals would prefer not to use: such as cutting corners in safety, or using child labour. And ultimately the world is too complex for any individual to make even very basic informed decisions, without reliance on others. Democracy and state is ultimately how the rules and conventions of that relationship is set. Trading information, such as paying for a consult, depends on the state to enforce honesty. And for those reasons, I sincerity think denying an industry regulation by state harms it overall. Usually doing so only benefits the already existing entities in that field. Without regulation, the commercial space industry can not form a honest market, and in some areas can’t have beneficial competition that drives innovation. It will remain highly risky, insurance companies won’t facilitate lowering the risks per-launch, and so few applications can make use of the services the industry can provide. Sure the companies can create more products more easily, but the products are much weaker without the structure state and regulations provide. It’s very shortsighted to point at the cheaper development costs, if they severe the value of the end-products by causing huge insurance costs and lower demand overall.
This is such a great argument against the common and incredibly simplistic view of ‘but the free market will fix it’. Without at least a third party arbitrator (which may be enforced through government) you can’t even have a free market.
Lol wtf are you talking about? Regulation only ever leads to regulatory capture and then no competition happens because the big players just pull the strings to regulate any would be competitors out of the market. Also, informed consent doesn’t have to mean “you know all of the details”, part of your informed consent can always come with the “bad shit we haven’t anticipated yet might happen, wanna go anyways?” You explicitly give consent to take unknown risks all of the time. It’s part of life.
@@banksuvladimir i like how your argument against regulation treats corruption of the regulatory body as just a natural, unavoidable part of the process. And if the big players are corrupting legislators then they should not be rewarded by not being subject to regulation. Also i'm wondering if you saw the same video as i did, the entire point is that known (to virgin galactic) information being kept from those who have to give informed consent precludes assessment of KNOWN risks. If nobody certified that the structure can handle the expected forces, and they won't tell me any details like material used and dimensions, then how can i give informed consent to the risk of a structural failure? For perspective, this isn't nitpicking about potentially unknown mechanics causing something unforeseen, it's about a company that skipped unmanned testing and is doing a bunch of non-industry standard things while struggling to beat the odds of russian roulette while being extremely tight-lipped on information required for a risk assessment of known risks (just trust me bro we value safety bro)
Most crashes involving fly-by-wire systems were a combination of pilot error and issues with sensors (the Rockwell X-31 and B-2 crashes come to mind, both caused by humidity in sensors/pitot tubes). It would be shocking if that F-35 crashed due to a fault with the flight control computer itself
Had I been betting when the concord started I would've thought "no way this is gonna be in regular use, much less 27 years". Safe is always a measurement of risk and initially that risk can appear higher in regions of unknown. That said, had Ocean Gate used a large steel sphere we likely wouldn't be talking about the risk of space tourism with such a critical eye. I do believe there is a way to make space tourism safe enough for regular use, but the jury is still out on if Virigin has achieved this.
Excellent video, my only critique is that the “security is a fly by wire system” panel in the 1968 paper is definitely Linus, not Charlie Brown. I think that might even be his blanket in the lower right!
Really love your breakdown of this and Oceangate from an engineers perspective, even if a lot of it goes over my head. It really make me appreciate the hard work and talent that goes into good engineering.
Excellent analysis as in your previous offerings. For anyone in the UK having watched Branson's "trajectory", none of this seems much of a surprise. The "astronauts" who have gone up so far or are planning to, until the inevitable happens and the exploded bits of machinery are swept up and quietly disposed of, presumably imagine that BOTH the NTSB and NASA have implemented some form of more-rigorous-than-normal oversight here, throughout what they assume to have been the lengthy and judiciously executed design and testing phases. For my part I'm not at all surprised the only thing NASA are really bothered about is what happens when the bits come crashing back to Earth. Regarding loss of cabin pressure at 80 km, does anyone even know whether there is some kind of pressurised oxygen supply (as on planes)? Though I'm presuming that the pressure there is so low than in fact the physiological consequences would be far beyond just needing pressurised oxygen: horrific death essentially involving the explosion of the soft tissues (lungs, eyeballs, etc.). So best not to dwell on such depressing eventualities: it might undermine the Astronaut Experience™.
I think they do have a pressurised oxygen supply. Whether occupants could survive several minutes exposed to vacuum is a question I'll leave to the biologists. U2 pilots wear a pressure suit and they fly at less than 1/4 the altitude.....that tells me all I need to know.
this is… a great video. Its entirely unbiased and doesn’t use subjective language. Thank you for somehow opening my eyes to the dangers of commerical subortial spaceflight while not making me hate it. Nice work!
Thanks. I actually consider this to be my 'worst' video since my channel took off because I think it's too opinionated (also I had a new mic and you can hear all my gross mouth sounds that I didn't know how to edit out back then).
It's not about cost saving or having a "cop out." Burt Rutan has always had a habit of trying to limit automation as much as possible in his designs, he believes that simplicity means "less things that can malfunction."
The lack of regulation that allows Virgin Galactic to thrive is starting to creep into everyone’s lives: web privacy, pedestrian safety and data consent laws are a few examples. I will do more videos on the matter in the future.
@@Alexander-the-ok Yep. The motto of move fast break things, pay regulatory fines later; Is a dangerous precedent to set in the transportation of people. At least digital tech generally doesn't kill innocent bystanders. Great Video so far
@okalex4687 Why not regulate those things and not hyperregulate people who want to explore, do research, or who simply find joy in riding to space? Everything has been so overregulated that we created a generation of people with diabetes, not much inclination to do much of anything in exploration, scientific research, etc. least they face fines, arrest, etc. It's incredibly sad and breaks my heart. Overregulated people are slaves.
@CarolReidCA If Virgin Galactic truly wanted to explore and do research, they'd have made their designs and findings public. Open source engineering data would be a good alternative to a third party (ie regulators) stepping in and pointing out that they may be deceiving their customers about how safe their system is.
Superb analysis and a joy to watch. You set a very high bar. I would certainly want to see the story of the F8 test plane which I assume is about the shuttle's computer. I think you may have described it as Apollo. BTW,, I'm sure you can get this down to 55 seconds with some careful editing to accommodate UA-cam's strong preference for shorts. (Perhaps today's glorious quest for the ultimate in concision merits an investigation in itself. I have a feeling that embracing impatience to the degree our society has won't end well for us.) 😉
It was actually the apollo guidance computer - amazing right? The results were then used to develop the fbw for the shuttle. I’m definitely going to make a video about it. I have no interest in making shorts (except for the occasional silly stuff). When properly discussing risk, brevity is not a priority. Oh and thanks for the kind words!
@@Alexander-the-ok I'll look forward to whatever you put out next. I should clarify that my loathing for one minute videos is impossible to exaggerate or to express politely. ☺
The Space Shuttle was estimated to have a loss of 1 in 100 flights before it flew, as history tells the first major loss was flight 25 & 107. So the real statistics were stacking up to being say 2 losses per 100 flights across a small fleet of craft. Compared to say the 1966 Soviet Soyuz is the most reliable with over 1900 flights, flown way more than the still baby Falcon 9. Virgin Galactic has a sniff of Ocean Gate going on, but so does a trip to the top of Mount Everest. Life's boring without taking massively expensive risks. Anyway imaging the bragging rights once you have survived such a risky adventure.
Reminds me of being a teenager and hearing a rumour that a kid died on a fairground ride. Stupid me and my friends would be desperate to go on that ride so we could brag ‘we survived’ it.
@@JohnWilliamNowak the last soyuz fatality was in 1968. It has gone through many design improvements since and now has a 55 year unbroken ‘non kill streak’
What a brilliant thought provoking presentation, thanks. It's probably a good idea from time to time to take a good long look at the risks we all take in our lives and decide what's acceptable and what isn't!
Thanks very much. I do get nervous when my videos get a lot of attention - two months ago I had practically zero online presence. But yes I agree, hopefully we'll see more content that goes against the overwhelmingly common view of 'wooo space tourism is the future' in the near future.
People need to assess risks for themselves, or we aren't free people. Let those who decide to go decide for themselves. If minors are involved, let that be up to their parents. Overregulation is killing people by turning people into couch potatoes, diabetics, anxiety ridden blobs, and so on. Heart attacks and diabetes kills slower, but they still kill people, after making them miserable.
@@CarolReidCA you can't be expected to be a expert in every single topic out there, some authority needs to be able to ensure products are safe because its frankly ridiculous for one to expect a average person(or basically anyone for that matter) to be able to accurately assess risk on all products and services they use.
@@CarolReidCAthis would be cool and all if the information required to accurately assess risk wasn't actively hidden. when someone decides to ride, they aren't assessing risk--they're either confident they'd be ready to die for the mission, or are actively mislead about the safety of the craft.
An outstanding piece of reporting and analysis. I am a longtime aviation/space writer and, being weary of VG's heedless rush toward disaster, did not expect to stay for more than a few minutes. In the event, I could not put down my tablet until you finished.
That is a hell of a compliment, thanks. I always think my analyses must be incredibly boring but sometimes that’s probably what the world needs - a boring assessment with no sales hype or speculation.
Too many factual errors in the video for me to take it seriously. You state that only three spacecraft in history flew without a LES, this is not true, Gemini, Vostok and Voshkod also had no LES. You could argue that Gemini and Vostok had ejection seats, but those were only usable the first couple of seconds in a launch. You also conflate hydraulic and fly-by-wire. Not all Hydraulic flight controls are fly by wire, and some hydraulic systems are even fully reversible. Many early supersonic jets have no fly by wire, they only have a normal, directly coupled hydraulic system, where the input on the stick directly relates to the position of flight controls. By your logic my 1980 Trabant has computer controlled fly by wire brakes, they are hydraulic and not mechanical after all. The idea that all early supersonic jets like the Mig-15, or F-105 were fly by wire is just laughable. It would not be until the F-16 that a supersonic jet would be all fly-by-wire. If a novice like me can point out these basic errors, that makes me doubt how credible the rest of the video is.
Alright lets address all of those: Ejection seats are a form of LES. I said ‘some kind’ of LES and even addressed the difficulties of supersonic ejection. I put a correction in about the hydraulics/fbw being ‘in everything’ at the 49 minute mark- i mixed up my words in the original recording. I didnt say the mig-15 or f-105, or ‘all early supersonic jets’ have fly-by-wire. I said they had non-reversible controls. Some earlier aircraft (like the x-15) also had analog fly by wire.
@@Alexander-the-ok Even if you include ejection seats (which, if former astronauts were to be believed, were pretty much useless anyway) you still have Voshkod, which didn't have an ejection system. It''s interesting that you mention the X-15's fly by wire system, since it had a mechanically coupled flight stick (this should mean it also was reversible, and if it wasn't please show me a source). The only thing the mh-96 adaptive flight control did was provide control to the RCS thrusters used when the plane high enough that air over the flight surfaces couldn't be used to control the plane anymore. This is more comparable to the fly by wire systems of early space capsules like gemini or apollo, then fly by wire on a plane. I'm not arguing that spaceflight is safe, rocket motors are no where near as reliable as other forms of propulsion, it still has a high failure rate, and passengers should know this. Even after 60 years we still haven't launched all that many humans. But I would go a virgin galactic flight if I ever had the chance, just knowing that there is a significant chance of death. People do things that are relatively high risk all the time, I was looking at undergoing laser surgery, and apperantly the failure rate is still nearly 1%. I'd rather wear glasses all my life then risk blindness, but I rather take a 1% chance of death to experience spaceflight, even if it's suborbital.
You are absolutely correct about Voskhod - I completely forgot about it. Thanks, I’ll pin a correction. Source for the X-15 controls here: bottom of page 6 www.nasa.gov/centers/dryden/pdf/87785main_H-618.pdf Anyway I think we broadly still agree on the main point here that spaceflight is dangerous and Virgin Galactic’s system is unusual and largely unproven.
These are trivial nitpicks relative to the major points of the argument sustained in this video. Go make your own perfect videos and let us know how that goes.
@@lukeybukey3081 No, I don't claim to have the time to properly research and make a video like this, so I don't. But if I, without doing that research, can already point out some inaccuracies just out of the top of my head, it always puts doubt that the author of the video did enough research, and is knowledgable enough on the subject to be a trustworthy source. Let's put it like this: If Scott Manley makes a video about this, I know he knows a lot more then me, and I will trust him to deliver accurate and factual information. If Drachinifel makes a video on warships, it's the same. If either of them made a video about let's say, architecture, and I can nitpick a couple of problems right away, I won't trust the rest of their points either, since their knowledge on the matter has been put into doubt. I might be more sceptical then I need to be, but I feel like that's something nessecary, since, while this video might make a point that is correct, so many videos on youtube are just full of people, fully convinced of being right, spouting nonsence.
Some corrections:
Thanks to @slome815 for pointing out there was one other launch system with no escape provision: Voskhod. I completely forgot about that one.
I said FBW was ‘the norm’ in 1968. That’s not correct. Irreversible controls were but fbw was in its infancy. There is a correction to kind of address it at 49 minutes and I’ll be doing an entire video about it in a few weeks. Thanks @SoloRenegade
For those unaware, Voskhod was the Soviet Union's second manned spacecraft. en.m.wikipedia.org/wiki/Voskhod_(spacecraft)
A future system also lacking a LES is the SpaceX Starship, though that project has such an array of fundamental issues facing It that I doubt that it will even fly freight to orbit.
@@Miata822 I've made the decision to only do videos on things that already exist (ie not CGI renders or half baked tests). If Spacex put humans in anything that even remotely resembles their starship proposals, I'll go there.
Gemini also didn't really have an escape system. Sure, they nominally had ejection seats, but a) Those would only be good for the first 40 seconds of launch, after that the spacecraft would be going too fast for the ejection seats that were fitted to be reliable, and b) I really do not like the prospects of firing an ejection seat charge inside a spacecraft that is pressurised to 1 atm with pure oxygen and has been soaking in that pure oxygen for over an hour prior to launch.
@@zuthalsoraniz6764 That's part of the design. The flash fire in the cabin as ejection motors fire helps precondition the astronauts and seats for the presumptive fireball they are ejecting into. /jk
Alexander: Every time you get in a vehicle you are, in effect, rolling a dice.
Oceangate: *flips coin*
The coin would have to be weighted for this to be an accurate analogy.
@@adriatic.vineyardsor the one-sided dice
A "die". Dice is plural
Dammit, I was gonna say the coin thing!
Just remember, the Karmen line is not fixed and arbitrary, but the Kerman line is unambiguously fixed and easily tracked by when the music changes.
Don't forget the Kerbal line also... 🤔
Ha! Ha! I LIKE K.S.P. TOO ! ! !😃😃😃😃😃😃😃
damn it jeb.
Ah yes, the Incompetech boundary.
Once you hear the "BWAH! (do do do do do do)", you've made it
One of the Mercury/Redstone engineers is still with us. He is 92 years old and comes to our shop for little machining jobs he can’t do in his home shop. Talked to him about meeting Wehrner Von Braun down in Alabama. He described the man as a skilled publicist and salesman as much as he was a scientist and engineer. Old Lyle is living history. Every time I see him is a bonus.
Absolutely fantastic. I'd be completely starstruck in the presence of him!
A Nazi is a Nazi but Von Braun was exceptional. He killed more people assembling his V-2 than did the business end of it. By the gods that is what it is about wasn't it, the eradication of the Jews. How soon we forget what the man did just so we could get to space. NEVER FORGET!
It is another sin this country has to endure that we didn't punish him and his countrymen, the greedy lot we are.
That's so freaking cool.
I was volunteering at a space museum this weekend alongside a 96 year old data reduction specialist who worked on the Snark program. He did a bit of work with computers to extract data for Von Braun when he was having trouble getting data in a timely fashion at Cape Canaveral, but only with the consent of Jack Northrop since that's who he really worked for (!). Fascinating, fascinating guy, really glad I got to spend some time with him this weekend.
My Uncle used to be one of Werner Von Braun's pilots when he was based in Alabama. (IOW, he flew one of the planes that Von Braun used to get around the country)
In the wake of Ocean Gate, any argument about a CEO's personal faith in product safety should ring especially hollow.
Actually, ocean gate has nothing to do with it one way or another. It’s one guy and one company.
Years of testing separate Virgin Galactic from Oceangate. If Titan tested as hard as Spaceship Two it would have imploded years before it started carrying passengers
There is one major difference: One of them knew what he was doing despite taking very weird and somewhat unsafe approach. Other was a rich idiot. One is alive, other is red mush.
@@theussmirage How has Musk tested his 'star ship'?
@@banksuvladimirit's one guy and one company, but one exception is enough to disprove the rule of "but the pilots wouldn't be in it if it weren't safe"
With respect to the "pilots wouldn't do it if it wasn't safe":
I know one of the astronauts who was on the return to flight mission after the Columbia shuttle disaster. He told me that the pilots and most of the astronauts (at least) would have gone up in a shuttle the next day if they had been allowed to.
They are probably more capable of understanding the risks of spaceflight than most people. They would have been willing to take the flight before anyone really even understood what happened. I would be willing to count that as "informed consent" but it had nothing to do with whether they believed it was safe (to the extent that spaceflight can be safe.) They understood the risks as well as anyone and decided it was worth it.
Many people would do these things despite them being unsafe, and that's fine, but for a layman to have informed consent, the risk needs to be appropriately characterized.
True.
To make a car compassion. I don't think any enthusiast wouldn't want to drive a F1 cat.
Problem is 95% wouldn't even be able to press the brake pedal hard enough to stop fast enough when actually going fast.
I’ve worked with many test pilots and a few astronauts and agree completely.
@@MyILoveMinecraft
The fastest I've gone on a highway is 152mph. If I could have gone faster I would have.
@@jackalopewright5343 They are just build different. Ready to push the limits whenever they allowed and approved.
@@Istandby666 Is your life worth that?
"I had been conditioned to believe that there is nothing more dangerous than the arrogance of ignorance; now I would learn that it does not compare with the arrogance of knowledge, knowledge that is often confused with wisdom." -John Piña Craven, 1959, on being appointed Chief Scientist of the US Navy.
That's why this channel has a silly name: to remind everyone that I'm just 'some dude' and I'm not particularly wise.
@@Alexander-the-ok😂
That's the same period of time that John Clark (author of _Ignition!_ (1972), a great technical autobiography of rocket fuel development) was running the rocket fuel lab at the US Naval Air Rocket Test Station (NARTS) for 17 years while avoiding any time-lost accidents. From some of the stories he tells, it was by careful understanding and caution when pushing near any sort of limit, whether knowledge or operation.
@@Alexander-the-okTotally love this idea! Though I'd still envy your reasoning & knowledge ;)
It's so true though. That's why they say "a little knowledge is a dangerous thing." What you think you know can get you killed.
Military systems engineer here. "Procedure" is *literally* the second to last choice for risk mitigation (the last choice being a placard, i.e., "YOLO - here's a sign to tell you to watch out for that!").
Same for any safety critical process in industry.
Depends on kind of person you're designing it for. I remember seeing something to the effect of "don't weld with ammunition present" on an ammo box on a US WW2 era warship.
@@sruz25cz This is what makes safety engineering in military systems so interesting to me as a civilian layperson. You can do all the traditional risk mitigation that you want, but to have an effective military you absolutely will need to put people with a wide range of backgrounds, education, and life experience directly in the path of some pretty dangerous situations even in peacetime. Finding where to draw the "we've done all that we can" line under such circumstances must be quite challenging, with some serious repercussions if you get it wrong.
I think you are forgetting PPE.
Elimination
Substitution
Engineering
Administrative
PPE
@@sketchyAnalogies I've always wondered about this hierarchy. Whether administrative or PPE are less effective controls depends a lot on context.
For instance, shoes are a form of PPE, but they're a much more effective control against foot cuts than a sign saying "sweep up all sharp objects". But administrative controls are definitely more effective in high risk cases. For instance, arc flash suits and ejection seats are absolutely the last line of defense.
The mirage III had hydraulic controls, but the stick was linked to mini-control surfaces in the middle of the delta wing giving back-force to the pilot
Oooh that’s cool, never heard of that before!
The parts manual for a 60-year-old jet that I deal with is approximately 16" thick. The maintenance manual is closer to 2 foot.
What's the jet? Just curious.
For all the bigger jets back in the day the AMM/IPC was all on microfiche for that reason; I've seen a full 747 AMM and it was something like I think 12 or 13 binders, each SUPER thick, like 6" thick. Literally 2 binders just for all the wiring diagrams
An Abrams tank is 4 dictionary sized books. And that's a ground pounder.
Just check out the binders that come with the manual for the IBM 5150
As someone with a passion for engineering this is the kind of content i crave. its a refreshing break from alot of the content out there that basically just reads off the wikipedia page.
also as a sidenote, ive also designed my own hybrid rockets and have recently been working on one basically the same as yours but i couldnt think of a decent way to break the nitrous cannister so thanks for that 😅
Ha! There are way better designs that use a meltable plastic disc and seals: you screw the canister down onto a spike to puncture it and it seals until the igniter melts the disk. I didn't bother with all that but I may in a future design.
My trust of transport platforms is now is based on the probability of an incident being followed up with the global engineering community collectively asking "well what did they expect?"
Yes, the CAA's AAIB (Air Accident Investigation Board) monthly bulletins made for some fascinating, funny and absolutely frightening reading.
If I’m fated to die in a transit accident, I aspire to at least avoid being a punch line.
When you mentioned Virgin hiring a frmr. Boeing exec I let out one horrified laugh knowing how buried important safety info would promptly become.
Same.
Yes if the media says Boeing is bad it MUST be true.
Alaska Airlines was warned about the door issue yet they are never mentioned. it's politics.
@@ExploringCabinsandMines That door was still attached when the comments you were replying to were written.
@@Neuttah oh really, I predicted the future? interesting....
@@Neuttah interesting...
Get ready to be summoned by Congress in 10 years to testify on Informed Consent. Great work 👏
Part of my day job involves compiling reports with data from engineers on failure probabilities. The numbers show certain things to be highly improbably ... until they occur. When calculating how many sides on the die, there is never enough information to really nail it down. Hundreds or thousands of hours of analysis sometimes is no better than a WAG.
In my world, even a tiny chance of something going wrong in a given hour gets multiplied by tens of millions of hours.
This is something I have to explain often in my job too: 'yes there's a one in a million chance, but we're going to run this 10 million times so it'll probably go wrong'.
Communicating this kind of risk can be really really difficult.
I think there's more need to test components to destruction in several different failure modes to have even a good WAG.
@@jackee-is-silent2938 Just when you think you've got all of the failure modes covered, the real world finds more. But there is literally a practical limit to testing; our last jet engine certification cost more than two billion dollars before a single product hit the market.
@@jackee-is-silent2938 and be so ungodly expensive that you'll never sell it. good intentions never work like you want. stop living in fear of death. stop being a bubble boy.
Yes. With enough opportunities, small probabilities become practical certainties.
When I was in Space Camp I asked what would happen if the explosive bolts didn't fire when the SRBs were ignited. The engineer who was talking to us just shrugged and went "The boosters tear them off and you launch anyway."
I always like to ponder what’d happen if the bolts only fired on one side. Obviously, hypothetical only since there were wired up in such a way to make that basically impossible. But fair to say the result would be…..a mess.
@@Alexander-the-okit would be a mess for sure, but that's the deal with solid rocket boosters. It's why I am always hesitant when it comes to grading safety on anything that relies on them.
If you encounter an issue during throttling up of a liquid engine you can shut it down. You can scrub the launch, or in the case of an in flight problem, you can fall back on any number of your other engines to pick up the slack.
You can't so that with an SRB. As soon as those light up, you are going to space, no matter if you want it or not, or if it will be in one piece.
@@mobiuscoreindustries The available evidence indicates SRB ignition can result in an apogee as low as 20 km. I wouldn't call that "going to space" when weather balloons regularly exceed 30 km altitude.
@@CoastalSphinx This is a way of saying. You cannot turn off the boosters, once they are ignited you have no other choice but to launch, otherwise you will likely cause a catastrophic failure on the launch pad. The boosters alone will not carry the vehicle to orbit of course but they are responsible for a large part of the thrust.
Now with a LES the crew may get out safely but its suboptimal for the infrastructure to be kinda forced to launch a rocket you know to be deffective because holding onto it would be so much worse
This is the type of content I can’t believe I get for free. Absolute class
Hello, loved the vid just popping in as a colourblind person to say I can't tell the difference between the yellow and green used in the Venn diagram. I get that it fits our established associations with the colours, but adding some sort of pattern marker would be huge in the future. Horizontal, vertical, diagonal, stripes or dots or something like that.
Oh man sorry about that! I had comments on earlier videos about font color but didnt think about it for the venn diagram. I’ll follow an accessibility guideline next time.
Am glad there are others. Red Green. -Clay
I think Alexander already gets this, but it's worth pointing out: The presence of an LES isn't important, what matters is how many failures and at what point in the mission will result in survival vs. death. If you focus more on the presence of a system than its capabilities, you can end up thinking ejection seats are a good idea in vertically-launched, vertically-landing spacecraft, for example. A proper escape system will be good, but it needs to actually be an effective design.
Absolutely a LES, or any other safety provision, is not a silver bullet.
Ejection seat can work in that system as well. And they are not a bad idea as 2-3 line of defence.
@@alexturnbackthearmy1907 I'd argue that they are a bad idea if it's vertically launched and vertically landing for a combination of factors
1. If it's vertically launched, astronauts will be on their backs, so they aren't going to gain altitude from ejecting. You can fix this with a big net, but it becomes more and more questionable that this is cheaper than a proper LES
2. Pressure suits don't provide protection against rocket exhaust or high-speed air. For example, the Space Shuttle is moving too fast for safe ejection after just 100 seconds
3. They add a bunch more things that can go wrong. Take that flight where the hatch blew off by accident on landing. If you need the ability to eject, the hatch needs to be fitted something like that, plus of course the rocket motors in each seat, which would have killed the other crew pretty quickly back when capsules used pure oxygen
4. Given the added weight and added complexity, I have my doubts that they are even all that much cheaper than a standard, tower-based LES, while offering much more limited capabilities and more failure points.
I'm glad you framed it in terms of informed consent rather than risk-taking per se.
What a superb feature: using well-researched and referenced information to build a compelling argument. It’s quite accessible, yet detailed. You’ve found a new subscriber.
Thanks very much - more on the way soon!
This is so much more elaborate than news outlets saying "oh it crashed😢", we need more of this type of content!
Yeah it's 2024 now. Just saying, if it's Boeing, I ain't going.
Excellent presentation! This thing is even more Kerbal than I originally thought. "Failure isn't an option, it's standard equipment" :D
Best of luck with your growing channel. You put a lot of work into this.
Thanks. Yep, read 3 books and a month of research, writing and editing for this one! Quality research takes precedence over upload schedule.
Really enjoying these deep dives. Thank you for the work you put in on this. "I do not care if operators are sued or not, this conversation is about safety." Lordy if I didn't end up walking away from a health and safety position when I realized all I was supposed to do was minimize liability. God forbid we actually make things safe.
Thanks. Yeah…..for better or worse, financial liability can be an incentive for good safety practices. But it’s really depressing to see much of the discourse after an incident being ‘I hope X gets sued’.
This is about science not some morbid false ideology in a non existent, non proven, sky daddy.
Religion and schizophrenia go hand in hand. Seek psychiatric help.
I liked my university's risk management department back when we were doing rocketry. We found a way for the liability and the safety to align, such that the university is happy, the safety people are happy, and we are safe and doing cool things.
Workplace safety, though? I have to essentially remind them that this email will look really bad in a lawsuit in order to get them to reorder PPE.
21:50 “Virgin Galactic hired a retired Boeing executive to conduct a safety review” Well that aged like sour milk 😂
I too, have always had concerns, when I've heard the statement "it must be safe otherwise the pilot wouldn't fly in it" as history books are full of stories about dead pilots. I do, however, believe there's a 99.9999% chance the pilot will do as much as humanly possible to avoid disaster. Germanwings flight 9525 is one of the reasons it's not 100%.
If anybody ever says, “the pilot wouldn’t fly it if it wasn’t safe,” remember Eric Brown, who was a good pilot, BUT insisted on flying the ME163, despite warnings from the German ground crew.
Great video! Have always found the Rutan/Virgin Galactic model/approach a bit sketch... Minor quibble, at 49:29, that's not Charlie Brown, that's Linus Van Pelt!
For what its worth, Virgin fired their chief test pilot because he reported an almost fatal incident during one of their test flights to a reporter at Washington post. Essentially, acting as a whistle blower. The RH horizontal stabilizer exploded during boost. About 40 seconds in if I remember correctly.
Anyways... their main oxidizer tank is growing weaker and weaker...
I took the footage used in your opening. There are some gaps and anomalies in the publicly available data about the 2014 crash. It is possible that something happened before the feather mechanism was activated, something that Alsbury was responding to. Nitrous can act as a monopropellant with a very energetic decomposition. If this happened inside the fuel injector valve it would have weakened the structure in a way that is consistent with the geometry of the breakup and with long range photography of the mishap.
I signed up, ready To Go!!!
Can't wait to see the Titanic in person!
Haha. This is the kind of quality I look for in the first comment on the video.
I work on liquid rocket motors and as i've heard a colleague of mine who worked on a previous hybrid rocket motor say- Solid rockets don't want to shut off, liquid rockets don't want to start, and solid rockets don't want to do either
Huh?
@@RENO_K The third phase should be "Hybrids don't want to do either." A hybrid's solid grain is difficult to light because you have to spray oxidizer across a large area and get that area ignited, needing a large, energetic pyrotechnic- a significant solid rocket motor in itself. Then when you cut off the oxidizer (either by running out or closing the ox valve) you have a large area of hot fuel grain that continues to evolve gas for a long time.
On the other hand, with a small liquid motor, I've tapped out Morse code just because I could :)
Civil engineer.. Love the video. I know you're specifically talking Virgin Galactic but overall a brilliant presentation that well summarizes the state of "safety" in the billionaire unknown-tourism industry (space/ocean/etc). I hope against hope we see more change towards understanding this way of thinking without more accidents happening first.
My degree is in civil engineering too actually. My main concern is this 'free market will solve safety' ethos creeping into everyone's lives - willing participants or not.
@@Alexander-the-ok If the safety failures are fear-inducing enough, they aren't wrong -- the free market will solve safety -- just look at commercial airlines. It's hard to imagine the NTSB being formed and the FAA being held to account without the profoundly fear-inducing media coverage of airline crashes. Sure, the safety improvements rely upon unwilling participants dying but over 100 years they did seriously improve the safety record.
Road traffic, on the other hand, is terrifying only if you understand statistics and safety factors. (I still get very anxious standing on street corners waiting to cross at busy intersections with vehicles traveling at 40 to 50mph, very high alert -- and predictable "accidents" every few months)
Does anyone care if billionaires ker-splat themselves seeking thrills or bragging rights?
@@stephenkalatucka6213 Even from that point of view plenty of common/poor people get caught up in disasters like the Titanic. If people volunteer themselves for Darwin Awards that is definitely their freedom.
The Apollo Computer F-8 sounds like an interesting story, but what I want to hear about even more is the MR-1 launch (or just mercury-redstone in general)
The F-8 digital fly by wire is fast becoming my favourite for next video.
I may do MR-1 in a ‘Christmas special’ of comical failures or something daft like that.
It was because of two cables separating in the wrong order. Because of this, significant power went through a relay which tripped a command since the control cable was supposed to separate first. The command was meant to separate the abort tower AND the booster from the capsule. To prevent the capsule from separating from an accelerating booster, the booster separation could only occur when the spacecraft was in ~0 g. Since it was on the ground, the sensors showed a booster accelerating by 1g constantly, so the abort tower was the only thing that jettisoned.
That's not all, though. The recovery parachutes also activated since the capsule was detected to be under 3 kilometers and so it thought it needed to deploy the parachutes. Since the recovery system detected no load on the parachute since the capsule wasn't falling, it deployed the reserve parachute as well. The capsule was undamaged and was reused for MR-1A, and the missile was sent back to huntsville for refurbishment and a potential flight in future, but was eventually placed on display.
MR-1 was about as close to disaster as that vehicle could get without exploding.
The amount I learned from this video about laws, planes, spacecraft, flight control systems, regulations, ethics, rocket engines, aerodynamics, systems design, automation and insomnia are exceptionally impressive.
Thank you for this wonderful presentation and previous presentations on submersibles along with the associated sources, plenty of things to dig into. I really look forward to future videos.
Thanks very much. There will be more on the way soon!
"This video is not a billionaire showdown" thank you so much for this haha it's getting really tiring to always hear about the billionaires who own the company when people report on space news
You don’t have a ton of subscribers yet. But your content reminds me of Perun, the defense economics UA-camr who blew up since the full scale invasion of Ukraine. I’m looking forward to when you do your 100k subs video and I can say I was there before 10k ❤
Perun is one of the main inspirations for my format. To be honest I'm amazed how many people already want to listen to me.
I literally had the thought watching perun of “damn this is good, but I wish I could get this for non defense engineering”, found your channel the same day. (:
@@Alexander-the-okyou're doing good work! If you keep putting out good stuff, people will want to watch it!
Calling them Astronauts and Mission Specialists is for the same reason they were Mission Specialists on the Titan. The informed consent rules are certainly different for "Crew" compared to "Passengers". The liability laws probably parse depending on if it is a 'customer' vs 'crew'. They are not calling them that just for marketing.
Except that entire statement is nonsense. The informed consent rules in this case are literally laws and regulations enforced by the FAA. They are literally just calling them that for marketing. SpaceShip2 is certified for human flight with passengers by the FAA.
To not have a fly by wire system with hydrologics or electric actuators is crazy at Mach speeds, just insane
😅
Perhaps the FAA has not demanded certification for Virgin Galactic nor Blue Origin because they are not in the business of *transportation*. Their sub-orbital craft are essentially glorified amusement park rides.
I mean, the FAA grounded all B-17’s over airworthiness, and 15 minute joy rides fall into the same category of “amusement park rides.”
Right now the FAA doesn't actually have authority to crew rate space vehicles, they apply the same rules to crewed and uncrewed launch vehicles (those requirements are higher than NASA's requirements for uncrewed but lower than their crew rating). NASA and the DoD both require and perform crew rating if you're working with them, but Virgin Orbit is isolated from Virgin Galactic so that doesn't apply here.
New Shepard is in a gray area since Blue Origin does do business with both, but has not flown crew for either. New Shepard is technically crew rated, having done all the tests required and meeting the requirements in principle (like having no abort black zones) but I don't think that NASA actually audited that testing because they've only shown interest in uncrewed launches for scientific instruments.
Great video,not sure why I clicked on this but I learned alot,love the Mercury Redstone 1 failure
Thanks. Yep I’m gonna have to talk about that more in a future video
Excellent presentation! With how few incidents there have been there's not much info or discussion of safety in space tourism. I think there will need to be more refinement of designs and procedures as it gets more mainstream with a larger customer base. Unlike air travel or extreme tourism "experiences" though it presents many unique challenges and may never reach the same level of safety.
That’s what drove me to making this video. There is virtually no critical analysis of VG. Almost everything I can find is blind optimism, nonsense about their stock price or advertising.
Absolutely brilliant content, like all your videos. Meticulous research and clear delivery. We appreciate this isn't a 2 minute job 👏🏼
"informed consent", by design, requires information to make a consensual judgement. Commercial secrets kinda sort of make this a bit tricky. One would have to be a bit of a nutter to go up in the thing, hey.
My very over-simplified solution would be ‘to be covered by informed consent you are required to open-source your design’.
Its problematic but a start. Companies that are allowed to operate without liability are essentially getting a free lunch.
You don’t need to be nutty, just misinformed. Most people, including me, don’t have the capability to do proper risk-analysis, let alone risk-analysis that takes to account gaps in knowledge or information.
It’s also worth stopping and considering how ridiculous knowledge over wide range of fields one would need to have to give informed consent to space flight.
Being able to consent without being properly informed means trusting some party based on reputation alone: and in this case the trusted party is the other side of the agreement…
@@catcatcatcatcatcatcatcatcatcaWhich is why it should be subject to certification process, meaning that a completely independent team of experts has assessed the risk.
Or you could all stop whining and realize that shit like this will happen when pushing boundaries in extremes. It’s absurd that you people want to grind the works to a halt over someone who chose to do a dangerous job dying. Faceless nobody blue collar workers die all of the time to keep things up and running and keep you air conditioned and comfortable. But when need to be forever bogged down in a ridiculous quagmire to try to prevent anyone from ever getting a boo boo while going to space
@@Alexander-the-ok several CPU design teams would no doubt agree and probably go up. On the other hand, several cryptography implementation teams would probably agree and still not go up in an open source space ship hehe
This channel went from interesting to my absolute most favourite channel on youtube.
From calculations and engineering done later, I think that the space shuttle having about 65 sides is optimistic, as many avenues of failure did not result in disaster due to a massive amount of luck.
Yeah I agree. Just going for 'nearest order of magnitude'!
The early space shuttle missions were later estimated to be between 1 in 9 to 1 in 25, but later missions with safety improvements put that up towards 1 in 100.
The NASA commercial crew program aims for a minimum failure rate of 1 in 300. That might be good enough for 4 flights per year to the ISS, one disaster in a lifetime, but I don't think that's what we are wanting if we are talking about space tourism. And I think Virgin might be around 1 in 20 right now, maybe 1 in 100.
The problem is that NASA failure estimates had absolutely no scientific validity. The numbers were just pulled out of their asses. That's why the program was ended. It was a boondoggle from the beginning, with no conception of how it was ever going to meet its stated objectives.@@phillyphakename1255
@@phillyphakename1255Your numbers don't correspond to real statistics
@@appa609 please elaborate
"I wish her and the other passengers the best of luck, though I do not know how much they will need."
Absolutely excellent closing statement! Really drives home how little is disclosed by the company regarding safety systems.
I hope potential passengers see this video.
I appreciate your professional approach to presentation of content - specifically, clear LIMITATIONS and disambiguization of "conflict of interest or endorsement"
Your structure adds to ease of understanding concepts. Keep up the great work!!
Mike Adam's accident was due to him experiencing vertigo and positioning the aircraft essentially perpendicular to its flight path while at high altitude... Hard to picture! Shortly after, while re-entering the denser atmosphere, the aircraft entered a spin as a consequence. The initial trigger was, as far as I remember, some kind of electrical failure that distracted him. But vertigo was the overriding factor. It was learnt after the accident that he had been prone to it during his initial flight on the X15.
I disagree. I led development on SS1 hybrid motor. Just from watching videos on UA-cam I believe it suffered some sort of valve anomaly. I had seen that type of anomaly phenomena before. Failure modes can vary. The end result is clearly much lower thrust. It’s clear to me that the video shows ignition was normal. Black smoke as the solid rocket motor starts the hybrid looks ok. The initial start looks normal. What follows is more serious. Videos make it clear that the rocket was never shut off successfully. I wish I could see the motor chamber pressure when Mike Asbury unlocked the pneumatic feather booms. The feather mode has saved the spaceship a few times at much slower speeds. It’s possible the crew saw increased nitrous pressure in the tank due to a valve fire. If Teflon seals were used, anything is possible depending on the design. From the video, it looks like the Nitrous is decomposing and burning something other than HTPB. Just a guess. I think the answer lies in the fluid flow system and the motor chamber pressure when the boom was unlocked as a way to slow the vehicle down and start dumping the nitrous. The vehicle was not designed to land with the full tank of nitrous. On SS1, I required the nitrous dump valve requirement to empty the tank in an emergency is under 2 minutes. The nitrous load full was 3000 lbs.
Note: I was not an employee of Scaled after SS1 went to Smithsoneon.
Great video. You did a good job of presenting facts in a non biased way. I agree with your concerns and cautionary assessments.
It is only a matter of time until there is a space tourism accident on par with what happened with the OceanGate Titan, and then people will start asking questions about the safety standards or lack thereof in the growing private space industry.
This channel is about to take off I hope. Incredible video. Love these long form projects
Thanks! By my definition it already has taken off. I had about 200 subscribers 4 months ago.
Another excellent video...I can really see this channel going places!
Great video, but I would have liked to see small clips of all of these crashes/launch failures spliced in as you talked about them.
I would have liked that too. Unfortunately no (public) footage exists of most of them. I didn’t feel it appropriate to show the 2014 incident
Just because Branson flew in Spaceship 2 doesn't mean Virgin Galactic has done adequate safety assessments internally. Rush chose to dive his Titan under similar conditions, and died in it.
It should also be noted that Starship doesn't currently have a planned crew escape system in its design, though that might change in the future.
Starship does not have a planned Launch Escape System but they also don’t plan to fly any humans on it before the number of uncrewed flights has reached into the hundreds. This buys down a lot of the risk.
@@TheMcspreader Starship could escape SuperHeavy only in very specific scenarios where they can throttle down most of SH’s engines. Otherwise it’s thrust to weight ratio is far far too low to out accelerate SuperHeavy. Also it can’t escape from itself and it’s far more dangerous itself than a capsule that only has a minimal number of engines.
@@Borodalf Correct. Starship's thrust-to-weight would have to astronomically improve to, say, escape a Challenger-type scenario. Being on the front of Super Heavy instead of hanging off the side isn't enough. Perhaps some extra internal SRBs on crew-rated Starships? Maybe even an ejectable crew section. Unfortunately, in the current design I don't see anyway not to at least take the header tanks with the crew section...
GOOD video. I've been waiting for someone to do a deep-dive like this for a long time, and got super excited when I saw your poll.
43:00 If the aircraft is actively nosing up to bleed velocity and extend range, that isnt a ballistic reentry. Ballistic is a reference to the parabolic path of travel (though, this of course is shortened by the atmosphere as seen with true ballistic reentries with Soyuz craft). If I'm not mistaken, the Apollo capsules technically weren't ballistic entries either due to the heat shield acting as a lifting body due to the angle of attack. Great video, though!
Yeah you’re right there, its only a ballistic arc until it hits the atmosphere again
You are so underrated and deserve more attention. I love space and technology and hope to see more content soon
Thanks. This video is getting a kind of ‘spiritual successor’ in a few weeks actually
This has been extremely enlightening. I'm really enjoying your work, keep it up!
oh hey it's dat plane boi
@@calebharris292 hi
Very interesting as always, hope you keep making these videos
The purpose of commercial spaceflight is not to benefit humanity. It is to generate profits for as little operating cost as possible. Nothing else.
Top notch content.
Understandable, Clearly and completely explained without dumbing it down.
Thank you.
1. They *have* a real VP of Safety?
2. Based on my private sector experience, no way in hell would I want to be responsible for safety at a private space company. The profit lust compromises everything, the need to please investors leads to pressure to overpromise and then cut corners trying to fulfill those overpromises.
Presumably you start in the job because it's a noble thing to try and keep the profit chasers in check. Then once you find out they can't be held back, you feel you daren't leave because of what you fear they might do if you weren't there.
Excellent video as always - I’m by no means an engineer so I always learn a LOT from your videos 👍🏻
At 32:15 - my guess is that passengers are referred to as “Astronauts” as part of a bid to avoid legal repercussions in case of a fatal accident á la the Oceangate titan implosion
I doubt it - I think it has more to do with ego stroking of the very wealthy who pay to ride. "Well if the company called me an astronaut, I must really be one!"
The reliance on "good pilots" as a security blanket has and will ever continue to cost lives, as has trusting the opinion of esteemed individuals such as Rutan without adequate risk assessment. Look at Apollo 1. After nearly drowning in the Liberty Bell 7 when the door inexplicably blew out on splashdown, I've read that the use of an inward-opening plug door on the Apollo capsule was one of Gus Grissom's (and other Apollo 1 astronauts') many demanded specifications for the crew module. And nobody was willing or able to convince him otherwise. It was going to be his craft to command and he was a national hero with unquestionably qualifying experience and credentials. He was truly a guy with "the right stuff" who had been there and done that in an era when almost nobody else had. But then came the plugs-out test and the fire and the door couldn't be pushed in or blown out. And Harrison Storms at North American Aviation was scapegoated for it, because who would even hint at a dead hero sharing any of the blame for his own death? Or that's how I read it. It's not like I was there. I've also read the astronauts suggested an outward opening hatch, which would conveniently absolve them of any blame, despite the inward opening hatch being included in Gemini craft. Not sure we'll ever know the truth.
Hybrid motors have a horrible tendency to spall off chunks of fuel that can get wedged in the nozzle causing a massive thrust asymmetry or worse over-pressure of the motor casing.
The McDowell line is the best line IMO to judge if you are in space or not. Great video!
13:25 - There has been one (or two) more suborbital crewed space flight not in your list. Notably, it was an *attempt* at orbital space flight, though. Soyuz 18a had an in-flight launch anomaly that caused the flight to be aborted (the third rocket stage lit its engines while still being attached to the second stage, so the Soyuz capsule engines fired to pull it away from way-off-target launch vehicle.) This capsule reached a height of nearly 200 km, more than high enough to be “a space flight.”
Although if we’re counting Virgin Galactic, then another in-flight-abort should be counted, too. Soyuz MS-10 experienced a similar launch booster failure, which caused it to separate. It reached 92 km of altitude, high enough for the 80km definition.
There was a third Soyuz crewed abort, but it was on the pad, so reached nowhere near space.
Amazing video. I have always been mystified by the lack of good info on these crafts, but just wrote it up to me not being too much of a space or aviation nerd to know where to look. But this explains so much.
When people use the "pilots do it" argument, they miss a very important point, those pilots are not average people they are test pilots, with who knows how many hours of experience and a death wish.
Let's differentiate that any risk has two independent factors, the inherent risk and the "if you stupid" risk. There are many people doing dangerous work, but as long as you stick to the rules you're very likely will be fine, but than again, there are special cases when you have both inherent and stupidity risk and need the truly unhinged who would happily sacrifice their own life just to help humanity progress a little bit.
Those scientist come to mind, who designed the ejection seat, and tested the human tolerance for G force.
Hats off to people like that.
Informed consent is a funny concept. In the last few years commercial tandem BASE jumping started popping up. None of the clients would do it if they had a clear view of the list of things that can go wrong. People just read "danger: death" and brush it off like they would read it in their car user manual.
In some sense, in specific areas of life, participation in democratic governance is the only form of agency individuals could ever have.
Private companies are at the mercy of each other, as the competition might reward strategies majority of the individuals would prefer not to use: such as cutting corners in safety, or using child labour.
And ultimately the world is too complex for any individual to make even very basic informed decisions, without reliance on others. Democracy and state is ultimately how the rules and conventions of that relationship is set. Trading information, such as paying for a consult, depends on the state to enforce honesty.
And for those reasons, I sincerity think denying an industry regulation by state harms it overall. Usually doing so only benefits the already existing entities in that field.
Without regulation, the commercial space industry can not form a honest market, and in some areas can’t have beneficial competition that drives innovation. It will remain highly risky, insurance companies won’t facilitate lowering the risks per-launch, and so few applications can make use of the services the industry can provide.
Sure the companies can create more products more easily, but the products are much weaker without the structure state and regulations provide. It’s very shortsighted to point at the cheaper development costs, if they severe the value of the end-products by causing huge insurance costs and lower demand overall.
This is such a great argument against the common and incredibly simplistic view of ‘but the free market will fix it’. Without at least a third party arbitrator (which may be enforced through government) you can’t even have a free market.
Lol wtf are you talking about? Regulation only ever leads to regulatory capture and then no competition happens because the big players just pull the strings to regulate any would be competitors out of the market.
Also, informed consent doesn’t have to mean “you know all of the details”, part of your informed consent can always come with the “bad shit we haven’t anticipated yet might happen, wanna go anyways?” You explicitly give consent to take unknown risks all of the time. It’s part of life.
@@banksuvladimir i like how your argument against regulation treats corruption of the regulatory body as just a natural, unavoidable part of the process. And if the big players are corrupting legislators then they should not be rewarded by not being subject to regulation.
Also i'm wondering if you saw the same video as i did, the entire point is that known (to virgin galactic) information being kept from those who have to give informed consent precludes assessment of KNOWN risks.
If nobody certified that the structure can handle the expected forces, and they won't tell me any details like material used and dimensions, then how can i give informed consent to the risk of a structural failure?
For perspective, this isn't nitpicking about potentially unknown mechanics causing something unforeseen, it's about a company that skipped unmanned testing and is doing a bunch of non-industry standard things while struggling to beat the odds of russian roulette while being extremely tight-lipped on information required for a risk assessment of known risks (just trust me bro we value safety bro)
This is so informative! Great job, fantastic reporting!🌻🌼🐝 Keep it up 🙌
On FBW systems: just a couple of years ago (2020) an F-35 crashed at Eglin AFB due to pilot error and some interesting fly-by-wire system behavior
Oh yeah, it happens. I’ll do a follow up about FBW in the future. Thing is, without FBW, the F-35 wouldnt be able to fly at all.
Most crashes involving fly-by-wire systems were a combination of pilot error and issues with sensors (the Rockwell X-31 and B-2 crashes come to mind, both caused by humidity in sensors/pitot tubes). It would be shocking if that F-35 crashed due to a fault with the flight control computer itself
I really appreciate that you have a limitations section
As a gay man, I find Blue Origins design to be... Delightfully erousing
You dont need to be gay to be turned on by that hydrogen/lox open cycle engine design.
@@Alexander-the-ok 😉
Had I been betting when the concord started I would've thought "no way this is gonna be in regular use, much less 27 years". Safe is always a measurement of risk and initially that risk can appear higher in regions of unknown. That said, had Ocean Gate used a large steel sphere we likely wouldn't be talking about the risk of space tourism with such a critical eye. I do believe there is a way to make space tourism safe enough for regular use, but the jury is still out on if Virigin has achieved this.
Excellent video, my only critique is that the “security is a fly by wire system” panel in the 1968 paper is definitely Linus, not Charlie Brown. I think that might even be his blanket in the lower right!
So it is! I don’t think ive seen a peanuts strip in my entire life so thats my fault for guessing
Really love your breakdown of this and Oceangate from an engineers perspective, even if a lot of it goes over my head. It really make me appreciate the hard work and talent that goes into good engineering.
Thanks. Yeah, engineers do a huge amount behind the scenes to keep us safe. I feel ok saying that because I’m not an engineer anymore!
Excellent analysis as in your previous offerings.
For anyone in the UK having watched Branson's "trajectory", none of this seems much of a surprise. The "astronauts" who have gone up so far or are planning to, until the inevitable happens and the exploded bits of machinery are swept up and quietly disposed of, presumably imagine that BOTH the NTSB and NASA have implemented some form of more-rigorous-than-normal oversight here, throughout what they assume to have been the lengthy and judiciously executed design and testing phases. For my part I'm not at all surprised the only thing NASA are really bothered about is what happens when the bits come crashing back to Earth.
Regarding loss of cabin pressure at 80 km, does anyone even know whether there is some kind of pressurised oxygen supply (as on planes)? Though I'm presuming that the pressure there is so low than in fact the physiological consequences would be far beyond just needing pressurised oxygen: horrific death essentially involving the explosion of the soft tissues (lungs, eyeballs, etc.). So best not to dwell on such depressing eventualities: it might undermine the Astronaut Experience™.
I think they do have a pressurised oxygen supply. Whether occupants could survive several minutes exposed to vacuum is a question I'll leave to the biologists. U2 pilots wear a pressure suit and they fly at less than 1/4 the altitude.....that tells me all I need to know.
this is… a great video. Its entirely unbiased and doesn’t use subjective language. Thank you for somehow opening my eyes to the dangers of commerical subortial spaceflight while not making me hate it.
Nice work!
Thanks. I actually consider this to be my 'worst' video since my channel took off because I think it's too opinionated (also I had a new mic and you can hear all my gross mouth sounds that I didn't know how to edit out back then).
I’m shocked by the lack of automation in this design and I think it’s a cost saving measure
An easy cop-out. Don't blame the dodgy craft, blame the dead pilot.
It's not about cost saving or having a "cop out."
Burt Rutan has always had a habit of trying to limit automation as much as possible in his designs, he believes that simplicity means "less things that can malfunction."
I'm really enjoying your videos. They are well researched and presented.
Oceangate 2: galactic boogaloo? I'll be eagerly waiting
Why would you call your customers astronauts when space tourist sounds so much cooler given what it is
Rich folks doing dumb FOMO adventures and dying in accidents..Meh don't care.
The lack of regulation that allows Virgin Galactic to thrive is starting to creep into everyone’s lives: web privacy, pedestrian safety and data consent laws are a few examples. I will do more videos on the matter in the future.
@@Alexander-the-ok Yep. The motto of move fast break things, pay regulatory fines later; Is a dangerous precedent to set in the transportation of people. At least digital tech generally doesn't kill innocent bystanders. Great Video so far
@okalex4687 Why not regulate those things and not hyperregulate people who want to explore, do research, or who simply find joy in riding to space?
Everything has been so overregulated that we created a generation of people with diabetes, not much inclination to do much of anything in exploration, scientific research, etc. least they face fines, arrest, etc.
It's incredibly sad and breaks my heart.
Overregulated people are slaves.
@CarolReidCA If Virgin Galactic truly wanted to explore and do research, they'd have made their designs and findings public. Open source engineering data would be a good alternative to a third party (ie regulators) stepping in and pointing out that they may be deceiving their customers about how safe their system is.
I’d agree, except that they keep taking perfectly good pilots and experts down with them.
Superb analysis and a joy to watch. You set a very high bar. I would certainly want to see the story of the F8 test plane which I assume is about the shuttle's computer. I think you may have described it as Apollo. BTW,, I'm sure you can get this down to 55 seconds with some careful editing to accommodate UA-cam's strong preference for shorts. (Perhaps today's glorious quest for the ultimate in concision merits an investigation in itself. I have a feeling that embracing impatience to the degree our society has won't end well for us.) 😉
It was actually the apollo guidance computer - amazing right? The results were then used to develop the fbw for the shuttle. I’m definitely going to make a video about it.
I have no interest in making shorts (except for the occasional silly stuff). When properly discussing risk, brevity is not a priority.
Oh and thanks for the kind words!
@@Alexander-the-ok I'll look forward to whatever you put out next. I should clarify that my loathing for one minute videos is impossible to exaggerate or to express politely. ☺
The Space Shuttle was estimated to have a loss of 1 in 100 flights before it flew, as history tells the first major loss was flight 25 & 107. So the real statistics were stacking up to being say 2 losses per 100 flights across a small fleet of craft. Compared to say the 1966 Soviet Soyuz is the most reliable with over 1900 flights, flown way more than the still baby Falcon 9. Virgin Galactic has a sniff of Ocean Gate going on, but so does a trip to the top of Mount Everest. Life's boring without taking massively expensive risks. Anyway imaging the bragging rights once you have survived such a risky adventure.
Reminds me of being a teenager and hearing a rumour that a kid died on a fairground ride. Stupid me and my friends would be desperate to go on that ride so we could brag ‘we survived’ it.
Soyuz has 151 crewed flights, two fatal with complete crew losses.
@@JohnWilliamNowak the last soyuz fatality was in 1968. It has gone through many design improvements since and now has a 55 year unbroken ‘non kill streak’
@@Alexander-the-ok 1971. That said, I agree with your point that Soyuz is a well-tested and mature system.
@@JohnWilliamNowak oh yep, 1971. Thanks
What a brilliant thought provoking presentation, thanks. It's probably a good idea from time to time to take a good long look at the risks we all take in our lives and decide what's acceptable and what isn't!
We focus on system design, communications and legislation only. Now we're speaking the same language.
This sadly needs a lot more attention in my opinion! Thank you for making an amazing video!
Thanks very much. I do get nervous when my videos get a lot of attention - two months ago I had practically zero online presence. But yes I agree, hopefully we'll see more content that goes against the overwhelmingly common view of 'wooo space tourism is the future' in the near future.
Good video, can't believe this operation hasn't been shutdown like Virgin Orbit 💀
Ironically, I believe Virgin Orbit was safer, had more innovation value and had it's place in a growing market.
People need to assess risks for themselves, or we aren't free people.
Let those who decide to go decide for themselves. If minors are involved, let that be up to their parents.
Overregulation is killing people by turning people into couch potatoes, diabetics, anxiety ridden blobs, and so on. Heart attacks and diabetes kills slower, but they still kill people, after making them miserable.
@@CarolReidCA Regulation is to protect the public (the majority of the time) *cough EPA
@@CarolReidCA you can't be expected to be a expert in every single topic out there, some authority needs to be able to ensure products are safe because its frankly ridiculous for one to expect a average person(or basically anyone for that matter) to be able to accurately assess risk on all products and services they use.
@@CarolReidCAthis would be cool and all if the information required to accurately assess risk wasn't actively hidden. when someone decides to ride, they aren't assessing risk--they're either confident they'd be ready to die for the mission, or are actively mislead about the safety of the craft.
An outstanding piece of reporting and analysis. I am a longtime aviation/space writer and, being weary of VG's heedless rush toward disaster, did not expect to stay for more than a few minutes. In the event, I could not put down my tablet until you finished.
That is a hell of a compliment, thanks. I always think my analyses must be incredibly boring but sometimes that’s probably what the world needs - a boring assessment with no sales hype or speculation.
@@Alexander-the-ok Yes that's exact;y what the world needs!
Virgin has been "Galactic" since 2000 but can't even achieve low earth orbit...
Starship?
alex the GOAT what u mean. stellar work on this one, and series so far as well
Too many factual errors in the video for me to take it seriously.
You state that only three spacecraft in history flew without a LES, this is not true, Gemini, Vostok and Voshkod also had no LES. You could argue that Gemini and Vostok had ejection seats, but those were only usable the first couple of seconds in a launch.
You also conflate hydraulic and fly-by-wire. Not all Hydraulic flight controls are fly by wire, and some hydraulic systems are even fully reversible. Many early supersonic jets have no fly by wire, they only have a normal, directly coupled hydraulic system, where the input on the stick directly relates to the position of flight controls.
By your logic my 1980 Trabant has computer controlled fly by wire brakes, they are hydraulic and not mechanical after all.
The idea that all early supersonic jets like the Mig-15, or F-105 were fly by wire is just laughable. It would not be until the F-16 that a supersonic jet would be all fly-by-wire.
If a novice like me can point out these basic errors, that makes me doubt how credible the rest of the video is.
Alright lets address all of those:
Ejection seats are a form of LES. I said ‘some kind’ of LES and even addressed the difficulties of supersonic ejection.
I put a correction in about the hydraulics/fbw being ‘in everything’ at the 49 minute mark- i mixed up my words in the original recording.
I didnt say the mig-15 or f-105, or ‘all early supersonic jets’ have fly-by-wire. I said they had non-reversible controls. Some earlier aircraft (like the x-15) also had analog fly by wire.
@@Alexander-the-ok Even if you include ejection seats (which, if former astronauts were to be believed, were pretty much useless anyway) you still have Voshkod, which didn't have an ejection system.
It''s interesting that you mention the X-15's fly by wire system, since it had a mechanically coupled flight stick (this should mean it also was reversible, and if it wasn't please show me a source).
The only thing the mh-96 adaptive flight control did was provide control to the RCS thrusters used when the plane high enough that air over the flight surfaces couldn't be used to control the plane anymore.
This is more comparable to the fly by wire systems of early space capsules like gemini or apollo, then fly by wire on a plane.
I'm not arguing that spaceflight is safe, rocket motors are no where near as reliable as other forms of propulsion, it still has a high failure rate, and passengers should know this. Even after 60 years we still haven't launched all that many humans.
But I would go a virgin galactic flight if I ever had the chance, just knowing that there is a significant chance of death.
People do things that are relatively high risk all the time, I was looking at undergoing laser surgery, and apperantly the failure rate is still nearly 1%. I'd rather wear glasses all my life then risk blindness, but I rather take a 1% chance of death to experience spaceflight, even if it's suborbital.
You are absolutely correct about Voskhod - I completely forgot about it. Thanks, I’ll pin a correction.
Source for the X-15 controls here: bottom of page 6 www.nasa.gov/centers/dryden/pdf/87785main_H-618.pdf
Anyway I think we broadly still agree on the main point here that spaceflight is dangerous and Virgin Galactic’s system is unusual and largely unproven.
These are trivial nitpicks relative to the major points of the argument sustained in this video. Go make your own perfect videos and let us know how that goes.
@@lukeybukey3081 No, I don't claim to have the time to properly research and make a video like this, so I don't. But if I, without doing that research, can already point out some inaccuracies just out of the top of my head, it always puts doubt that the author of the video did enough research, and is knowledgable enough on the subject to be a trustworthy source.
Let's put it like this:
If Scott Manley makes a video about this, I know he knows a lot more then me, and I will trust him to deliver accurate and factual information.
If Drachinifel makes a video on warships, it's the same.
If either of them made a video about let's say, architecture, and I can nitpick a couple of problems right away, I won't trust the rest of their points either, since their knowledge on the matter has been put into doubt.
I might be more sceptical then I need to be, but I feel like that's something nessecary, since, while this video might make a point that is correct, so many videos on youtube are just full of people, fully convinced of being right, spouting nonsence.
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