SLS Evolution: What are the SLS Blocks?

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  • Опубліковано 7 чер 2024
  • Today we will be diving into the Block System of the SLS rocket! what are the SLS blocks, and what are their purposes? All that and more will be explained in todays video!
    Socials:
    Twitter: / davidwillissls​
    Discord: / discord
    Insta: / david_willi. .
    Credits:
    Music:
    Rebirth by Peyruis / peyruis
    Creative Commons - Attribution 3.0 Unported - CC BY 3.0
    Free Download / Stream: bit.ly/al-rebirth
    Music promoted by Audio Library
    • Rebirth - Peyruis (No Copyright Music)
    Intro (0:00)
    What is a Block? (1:04)
    SLS Block 1 (1:41)
    SLS Block 1b (3:44)
    SLS Block 2 (7:56)
    Conclusion (10:48)
    Outro (11:15)
  • Наука та технологія

КОМЕНТАРІ • 156

  • @DavidWillisSLS
    @DavidWillisSLS  Рік тому +26

    Sorry it’s been so long since my last video. But I’m back now!

  • @innosam123
    @innosam123 Рік тому +50

    It would be nice to see you talk about some of the proposed SLS launch versions, like Block IA (Advanced Boosters with ICPS), Block 0 (no 2nd stage), Block III (5-engine core) and the Dynetics LRB SLS.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +18

      I’ll save that for its own video, how about that?

    • @innosam123
      @innosam123 Рік тому +7

      @@DavidWillisSLS Nice.
      I forgot about the J2-X/high-thrust 2nd stage as well, which would work really well if we wanted to replace the ISS.

    • @OlCrunch
      @OlCrunch Рік тому

      @@innosam123 given that NASA is auctioning off J-2X, I don’t think that’ll ever happen sadly.

    • @HonoluluFireResponses
      @HonoluluFireResponses Рік тому +1

      @@innosam123 Earth Departure Stage?

    • @innosam123
      @innosam123 Рік тому

      @@HonoluluFireResponses Well, an earlier version of it.

  • @lewismassie
    @lewismassie Рік тому +11

    My favourite fact about the block IB SLS is that it has Saturn heritage. The Saturn I S-IV second stage was 5.5m in diameter. Over the years 5.5m tanks have been suggested for both Shuttle Boosters and the Ares-I second stage. The EUS oxygen tank is 5.5m in diameter.
    The block system is a really clever way to get around some of the limitations of govt-funded development. In such a thing, peak funding is the limiting factor. By spreading the peak funding between multiple waves, you can get bigger and more powerful rockets at the cost of time

  • @claimxart
    @claimxart Рік тому +8

    loved this video, I'm glad to see people showing more love for sls

  • @kommandantgalileo
    @kommandantgalileo Рік тому +9

    Note: one of the reasons the RS-25E is better is because it's gimbaling range is lowered, meaning it has less weight.

  • @TheSpaceflightGuy
    @TheSpaceflightGuy Рік тому +1

    Very good explanations! Keep up the good work!

  • @firefly2806
    @firefly2806 Рік тому +3

    I'm so hyped for the launch!

  • @jewymchoser
    @jewymchoser Рік тому +3

    As always, I love your content, hate the loud background music 🥲
    But thanks for posting, always a treat!

  • @nedodo2380
    @nedodo2380 Рік тому +2

    Can’t wait for the launch! Gonna be epic.

  • @kolesglock
    @kolesglock Рік тому

    Thank you for this an amazing video!!!

  • @epicdaniel508
    @epicdaniel508 Рік тому +4

    SLS Launch HYPE!!!

  • @TJCooney
    @TJCooney Рік тому

    great work David!

  • @bocachicacrane762
    @bocachicacrane762 Рік тому +2

    Great video David!

  • @lbdc8537
    @lbdc8537 Рік тому +6

    Good video! Although when showing numbers (3:26, 7:33, ) it would be good to slash height and thrust units in metrics, as some viewers can not be familiar with the imperial system of units. I also want to say that it is really nice to have you! You explain well the reasons why NASA will upgrade the rocket and everything behind the SLS. Oftentimes, I find that NASA communication doesn't explain very well the technical reasons behind the changes.
    Q: I didn't knew that the OMS stackover of the Shuttle will run out by Artemis 6. Given it is used on the ESM, will it be replaces by another motor or will a industrial develops a new Service Module? I guess NASA still wait for more Artemis mission before making a choice?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      Thank you! And yes, a new engine will replace the OMS, but from what I know it will pretty much be identical to the shuttle oms but with minor modifications

  • @hussarregiment7045
    @hussarregiment7045 Рік тому +4

    Big Orange Rocket goes brrrrr

  • @mactherebellionleader5394
    @mactherebellionleader5394 Рік тому +1

    Wow, that was fast, thanks so much!

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +2

      Tried my best! Hope you enjoy!!!

    • @mactherebellionleader5394
      @mactherebellionleader5394 Рік тому +1

      @@DavidWillisSLS I just finished it, its very informative and well researched, also, on a side note, do you play KSP?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +2

      I do play KSP! Yes! And thank you!!

    • @mactherebellionleader5394
      @mactherebellionleader5394 Рік тому

      @@DavidWillisSLS No problem, I hope you are able to expand your channel more, you have a lot of potential!

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      @@mactherebellionleader5394 thank you!

  • @pygzig
    @pygzig Рік тому +6

    Boeing has also been looking at producing carbon composite EUS tanks, which would reduce the weight of the stage significantly and would increase the SLS's lift capacity to be in the ballpark of Constellation's Ares V.

  • @edki669
    @edki669 Рік тому +1

    LETS GOOOO SLS

  • @allgood6760
    @allgood6760 Рік тому +2

    Artemis 1 was a success and now we are going back to the Moon to stay 👍🚀

  • @plainText384
    @plainText384 Рік тому +2

    For me the 10m fairing option on SLS Block 2 is probably among the most exciting things about SLS. Imagine what kind of telescope we could fold up in there. The JWST needed to fit in Arianne 5 with a 4.57m diameter space inside the fairing, it folded out into a 6.5m primary mirror.
    The Luvoir A concept would fold a 15.1m mirror into a 8m fairing.
    What kind of monster could we pack into a 10m fairing? 18m? 20m?

    • @stekra3159
      @stekra3159 Рік тому

      After finaly spending an other aircarfcarry worth of cash on a space telescope.

    • @_apsis
      @_apsis Рік тому +1

      @@stekra3159 more worth it than an aircraft carrier tbh

  • @RS-68
    @RS-68 Рік тому

    Can‘t wait to see the Block 2! It is the most powerful rocket in NASA history!🥳

  • @pawlitopawbur417
    @pawlitopawbur417 Рік тому +1

    David Willis, I think you have to edit the description of the video because there are no Music names and no Credits (i really would like to know what is the name of this music from the beginning of the video)

  • @iamarokotmanson
    @iamarokotmanson Рік тому +2

    SLS Block 1 cargo looks absolutely cursed

  • @MrTsukasashioten
    @MrTsukasashioten Рік тому

    very nice explanation!
    btw, what's the bgm? sounds so cute and fun haha

  • @rustyshackleford234
    @rustyshackleford234 Рік тому +1

    I can definitely see the block 1B launching, since congress loves the idea of a lunar space station, and the 1B can carry a crew and a piece of the station.

  • @Sam_Sam2
    @Sam_Sam2 Рік тому +2

    Fun fact the roll out will be on my 14th birthday :D

  • @manhdungnguyen5727
    @manhdungnguyen5727 9 місяців тому

    W

  • @cynbloxy
    @cynbloxy Рік тому +1

    I heard that there's a chance NASA will use two upper stages for Block 2, one which is the EUS we all know about and other which is way more powerful but less propellant efficient
    Great video btw

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      Thank you!

    • @innosam123
      @innosam123 Рік тому +2

      Is it the J2-X or something else?

    • @cynbloxy
      @cynbloxy Рік тому

      @@innosam123 we don't know guess it's J2X since it's the easiest to develop because rocketdyne has everything to continue development since it was halted in 2013

    • @innosam123
      @innosam123 Рік тому +2

      @@cynbloxy The only other one it could be is BE-3, but after the proposal was made, no progress has been made.
      Considering the nightmare the ‘commercial’ manned lander and spacesuit has been so far for NASA, it’d be silly to replace the 2nd stage with a commercial 2nd stage after EUS already is partially finished.
      Also, BE-3 is less efficient- and AR has the also mostly-finished RL-60 lying around, which was designed to have 4 times the thrust with similar efficiency and size (and was proposed for the SLS as well).

  • @masch2
    @masch2 Рік тому +1

    rad

  • @kludgedude
    @kludgedude Рік тому

    Can’t we get to 10 million lbs thrust at launch?

  • @louisr6560
    @louisr6560 Рік тому +1

    Thanks for the cool video! Impressive technology, however sad to see it mostly wasted on that questionable Lunar Gateway project.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +3

      Thank you! But Trust me, gateway is necessary for a sustained lunar presence

    • @louisr6560
      @louisr6560 Рік тому

      @@DavidWillisSLS Maybe, but I personally fail to see any real scientific benefit from a sustained (human) lunar presence, that could not be achieved by a much cheaper rover. On the other hand just imagine what amazing deep space missions you could achieve with just a fraction of the Artemis budget and all that payload volume!

    • @_apsis
      @_apsis Рік тому +1

      @@louisr6560 lunar mining and industry would be insanely beneficial to further space development, something that can’t be set up and done with a simple rover

    • @kingofaesthetics9407
      @kingofaesthetics9407 Місяць тому +1

      ​@@louisr6560Spoken like a true bean counter.

  • @anthonyhunt701
    @anthonyhunt701 Рік тому

    It’d be nice to see Block 2 take Dynetics Alpaca to the Moon ( Angry Astronaut asked the guys if it’d fit… they think so👍🏻🤘🏻🚀

  • @lownote711
    @lownote711 Рік тому

    Can we really say that Block2 has no heritage to the shuttle? Seems like a stretch to fit into a narrative. Thoughts?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      Not a stretch at all. Everything that would’ve come from the shuttle is gone. That’s how block 2 is defined

  • @AeonExploration
    @AeonExploration Рік тому +1

    Will the B1B maiden flight be crewed, or is it a test flight type mission?

  • @_mikolaj_
    @_mikolaj_ Рік тому +1

    Block 2 is inevitable, you cant run away from it no matter how much you questioned it, it will always come ;P
    EDIT: Bout block 2, isnt it supposed to have RS-25F eventually?

  • @dankatkov6133
    @dankatkov6133 Рік тому

    So its finally launched on november 16 2022

  • @brianchan8
    @brianchan8 Рік тому +2

    How far along is “why is sls not reusable part 2” at?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +3

      I’ve actually kinda forgot went about that 💀

    • @brianchan8
      @brianchan8 Рік тому +1

      @@DavidWillisSLS did you un-forget?

  • @Shadow_The_Pad
    @Shadow_The_Pad Рік тому +1

    I may not like the politics involved, but gosh I'm so excited for Artemis I!

    • @Shadow_The_Pad
      @Shadow_The_Pad Рік тому

      I may not like the politics involved, but gosh I'm so excited for Artemis II!

    • @_apsis
      @_apsis Рік тому

      @@Shadow_The_Pad why did you comment the same thing under your own comment 5 months later

  • @stekra3159
    @stekra3159 Рік тому

    We ride to the moon in a firy Typhon. On solide fule and wire. Turn the Key and light the fire we leaving earth to day.

  • @Ashie690
    @Ashie690 Рік тому

    Anybody got a link or name and creator for the name of the first music used in the video?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      It’s called “mood” and can be found in the UA-cam audio library

    • @Ashie690
      @Ashie690 Рік тому

      Ah , thanks a lot!

  • @erykpakula
    @erykpakula Рік тому

    How many ICPS exist?

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      3. 1 is in space. One is finished. And one is still being built. Those are the only 3 NASA will ever use

  • @JenkinsStevenD
    @JenkinsStevenD Рік тому +1

    Some of the information in here is not quite correct. The SRBs and RS-25s aren't "tHe ExAcT sAmE" for example. Space shuttle at liftoff was 7 million pounds of thrust. You don't get 1.8 million extra pounds of thrust from just adding one RS-25. Second, the block 1 has different sub-configurations as do the others. Those configurations are certainly more similar than they are different, but there are major differences internally.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      You get 1.8 million lbs more thrust by adding 1 more RS-25…. AND 2 extra SRB segments
      What sub configurations? Other than cargo NASA has released no other configurations for SLS

    • @JenkinsStevenD
      @JenkinsStevenD Рік тому +1

      @@DavidWillisSLS By the way, I like your channel. Lot of good videos and content.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      Thank you!

  • @DougGann
    @DougGann Місяць тому

    Has anyone actually figured out how the new ULT is supposed to work yet? Better delay that block 1B launch until we throw 10 years and 20 billion dollars at it.

  • @idk_itsme.
    @idk_itsme. Рік тому

    SLS launched already

  • @Fhcghcg1
    @Fhcghcg1 Рік тому +2

    It almost seems like it would have been cheaper and quicker to just put all the original Space Shuttle hardware in a museum and skip straight to the block 2
    I guess that’s just not possible with politicians in charge tho

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +2

      cheaper in the long run, but far far far more expensive each funding round. which is what gets programs cancled

  • @bambinazo123
    @bambinazo123 Рік тому

    Then
    It goes even further beyond and becomes reusable like Vulcan

  • @isuruanuradha2222
    @isuruanuradha2222 2 місяці тому

    Try to disappeared all I T app this lsland

  • @user-ec5rh7ep1e
    @user-ec5rh7ep1e 10 місяців тому

    Jolkosun

  • @MustafaKemal-oe8ie
    @MustafaKemal-oe8ie 19 днів тому +1

    I think NASA wont build the block 2 because it is too expensive. The block 1 is already a diet for the wallet

  • @VicariousAdventurer
    @VicariousAdventurer Рік тому

    The SLS has not been around the Block yet

  • @AerospaceAdler
    @AerospaceAdler Місяць тому

    Wait when SLS 1B will be flying i will be out of school. Fu- ..

    • @DavidWillisSLS
      @DavidWillisSLS  Місяць тому

      Around 2028-29

    • @AerospaceAdler
      @AerospaceAdler Місяць тому

      Yeah i know . Thats when i will be out of school. I better learn some patiance to see my Favorit rocket fly

  • @planetsec9
    @planetsec9 Рік тому +3

    The EUS is the most underrated aspect of the SLS Program IMO, there may not even be a need for a Block 2 with that thing around. NASA should try to make it refuelable in orbit, maybe add those new RS-25E's to it to swap out the RL10's and then have a monstrous amount of delta-v and C=3 available for outer solar system or interstellar payloads. Maybe they can even stretch the EUS for that purpose for even more performance and launch it on Super Heavy instead of SLS therefore saving all the development money/effort on a new Block 2 and instead maximizing the ROI on EUS, and allowing them to make more EUS' per year to launch more stuff.
    I swear I'm more of a fan of the EUS than the SLS at this point, I mean when was the last time NASA had a dedicated hydrolox upper stage that could be this versatile and have this much potential, not since SIV-B and even that was 6m while EUS can have a 8-9m fairing, go EUS!

    • @planetsec9
      @planetsec9 Рік тому +1

      Correction- Saturn V S-II was the largest hydrolox upper stage, 10m with J-2 engines

    • @sirmicro
      @sirmicro Рік тому +2

      It takes 4 RL10s to make 100k lbs of thrust, a single RS-25 makes 500k lbs thrust and can throttle down to 65% or so. I think you'll be crushing the payload with an RS-25 when the tanks are near empty...

    • @dr4d1s
      @dr4d1s Рік тому +3

      ​@@sirmicro Exactly. And when you have a powerful core stage with giant srbs it makes more sense to pair it with a low thrust, high efficiency engine. That allows you to achieve really precise insertions that can be more difficult with a monster like the RS-25 and save lots of propellant in the process. Not that the RS-25 can't do those things, it just makes it more challenging. Use the correct tool for the job at hand.

    • @lbdc8537
      @lbdc8537 Рік тому

      In addition of what Cody Ruthko said, there is also the question if the RS-25 can be turned on in space. Remember, on the Shuttle and SLS, first stage's RS-25 are turned on with the help of a little hydrogen on the launch pad. But yeah, go EUS!

  • @ericliu5491
    @ericliu5491 Рік тому

    Hope NASAs Mars vehicle will be reusable.

  • @joshuazelinsky5213
    @joshuazelinsky5213 Рік тому +6

    Well done. This was a good explanation.
    It seems unlikely that SLS block 2 is actually going to fly. The cost per a launch is massive, and by the time would be flying at the earliest, it is highly likely that SpaceX's Starship will be flying, and even without that Blue Origin's New Glenn will also be flying, and although NG won't have the same lift capability as SLS, the sheer cost difference would by itself make a massive difference. I'll be surprised if block 2 flies.

    • @hussarregiment7045
      @hussarregiment7045 Рік тому +4

      The thing is that Starship and New Glenn need to prove commerical viability if they want to last long. If either are unprofitable to run then they'll die. SLS doesn't have this problem.

    • @joshuazelinsky5213
      @joshuazelinsky5213 Рік тому

      @@hussarregiment7045 That's true, but commercial viability here shouldn't be that hard if they can actually work. If Starship can do second stage reuse, then it will likely quickly become cheaper than any rocket which isn't doing at least single stage reuse for even very small payloads. And NG is being built to be efficiently and cost effectively reusable from the ground up. (If I were to guess a problem with NG, it would be that reuse for it turns out to be harder than they expect, or they end up losing more than they were expecting early on.) And of course, there are all the other new rockets coming online also (see for example, Tory Bruno's comments about the possibility of a Vulcan Superheavy).

    • @hussarregiment7045
      @hussarregiment7045 Рік тому +10

      @@joshuazelinsky5213 The thing is this is all built on hypotheticals, if Starship can achieve reuse, if it can have high turnaround, if it can refuel at the scale it needs to, if is cost-effective. None of this has been proven yet, and frankly I do have my doubts about 2 of these.
      However another thing is that SLS Block 2 has something no other rocket her can do send 46+ tons on TLI in one launch, at best Starship will need 10 if you believe Elon Musk, althouth it's probably 14-15. And unless you're using Elon numbers (5 million dollars to refurbish and get ready for another launch in 3 days) then I don't see how it's more cost-effective than SLS Block 2.

    • @_mikolaj_
      @_mikolaj_ Рік тому +3

      Not really, all they need to do is fly SLS 10 times, and afaik, Block 2 boosters are already in development and their components will be implemented into B1B flights over time.
      Recent FSB-2 test on July 21st had some Block 2 parts
      Arguably the largest and probably hardest thing to make for block 2 will be composite casings for the motors

    • @cube2fox
      @cube2fox Рік тому +1

      I agree SLS Block 2 will never happen. By that time it is highly likely that Starship will be available. If NASA really needs a lot of payload launched in one go without refilling for some reason, they could even use Starship in a partially or fully expendable mode. That won't be cheap, but probably much cheaper than developing (and launching) SLS Block 2.

  • @simplex7096
    @simplex7096 Рік тому

    SLS is DOA

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому

      Well it arrived 2 months ago, and it’s still the most powerful and most capable operational rocket we have. So DOA it is not

    • @simplex7096
      @simplex7096 Рік тому

      @@DavidWillisSLS you forgot to add the most expensive

    • @AerospaceAdler
      @AerospaceAdler Місяць тому

      Saturn V was close if not evan more expensive per launsch and its development was 3 times the cost of SLS

  • @_K3PLR
    @_K3PLR Рік тому +1

    Im not exactly sure if we'd see block 2, Id expect for the commercial industry to take over in launch services by that time, which would free up quite alot of cash for NASA

    • @iamarokotmanson
      @iamarokotmanson Рік тому

      Almost definitely. Orbital refueling will make it completely unnecessary

    • @innosam123
      @innosam123 Рік тому +6

      No it won’t.
      Starship is a joke, and the proposals for commercial manned lunar landers are
      1. As expensive as those planned by the government (Altair vs commercial landers costs) when you account for the 2 models.
      2. Require construction from multiple launches that add up to ~600mil (vs $1B for SLS)
      Also, SLS has a limited supply of Shuttle components that require the advanced boosters to replace, as the old Shuttle SRB factories are long dead and will not be reopened (they use outdated steel casings for the SRBs, which have long since been replaced by GEM-type casings.

    • @iamarokotmanson
      @iamarokotmanson Рік тому

      @@innosam123 how does that make SLS Block 2 not unnecessary? You're just saying completely unrelated stuff

    • @iamarokotmanson
      @iamarokotmanson Рік тому

      @@innosam123 Altair was supposed to be $12b, ALPACA is $6b and the Old Guard was $10b. Starship is $3b

    • @iamarokotmanson
      @iamarokotmanson Рік тому

      @@innosam123 how is that an argument for SLS B2?? You just proved distributed launch is better and cheaper

  • @skeelo69
    @skeelo69 Рік тому

    NASA's SLS Rocket is about to finally Launch ............................................. Um.......................Nope.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +2

      Y’all are actually a bunch of babies if you get upset over a scrub

    • @codymoe4986
      @codymoe4986 Рік тому +2

      Well this sure aged like a glass of milk, left on the countertop...
      Tune in tomorrow morning to watch Orion flyby the moon, courtesy of a lift from SLS...

  • @jamess.8223
    @jamess.8223 Рік тому

    NASA is going to have a difficult time funding this beyond Artemis III. Private company's are going to win in the long run.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      NASA doesn’t have to worry about funding it because congress wants it. It doesn’t matter if there are alternatives. Those alternatives don’t come with the same benefits outside of spaceflight that SLS does

  • @Andreas-gh6is
    @Andreas-gh6is Рік тому

    SLS is too big to fail... If it fails tomorrow the whole Artemis program could be finished.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      Yup. That’s why it’s very likely that the launch will be scrubbed. Slim chance this thing goes on it’s first try

    • @AllThingsSpace3
      @AllThingsSpace3 6 місяців тому

      @@DavidWillisSLS Artemis 2 is in 12 months

  • @jaimeduncan6167
    @jaimeduncan6167 Рік тому

    Too expensive to get in the 30s a rocket that barely surpass the Saturn V. This rocket can't compete with the upcoming Chinese rockets and using hydrogen from the first stage makes little sense.
    For the. time and the amount of money that it toke it had been better to create a new first stage and use the Delta IV less expensive rocker engines for the second stage (with an extension) and get a 90t to lunar orbit. The other option was to take into account the years NASA has on space assembly and use multiple launches to create a modular system for the Moon program.

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +1

      SLS does not take any more money per year than the space shuttle did, and has more congressional support to boot. Cost is a non issue

  • @mamitomoe321
    @mamitomoe321 Рік тому

    I want this to succeed, but I'm having doubts. I don't think NASA would be able to recover financially if this goes wrong. If this fails, we can say goodbye to NASA. Thank the smoothbrains in congress for not giving them an acceptable budget.

  • @karlfreiha4745
    @karlfreiha4745 21 день тому

    Lbs of thrust ? bro ut talking about science please use the metric system dont be like that ... if you were doing a video on real estate in the usa okay no problem but really ? here dude?

  • @FoxBoi69
    @FoxBoi69 Рік тому

    very bold of anyone to assume sls will fly past the mid 2030s. i hope we will see it fly for decades, but i don't think it will be competitive enough. once other rockets such as starship or new glenn have been proven reliable, there will sadly be no point in keeping sls around

    • @tonk2629
      @tonk2629 Рік тому

      Starship and new glenn are cargo rockets, they’d have to make completely new lunar capable capsules

    • @FoxBoi69
      @FoxBoi69 Рік тому

      @@tonk2629 starship is a cargo rocket but with the end goal of sending humans to mars. let's see what spacex makes of it

    • @tonk2629
      @tonk2629 Рік тому +1

      @@FoxBoi69 The starship, in its current form, and even in future forms, is not fit to send humans to mars.

    • @FoxBoi69
      @FoxBoi69 Рік тому

      @@tonk2629 starship is in early prototyping

    • @gotanon9659
      @gotanon9659 Рік тому

      ​@@FoxBoi69 This comment age very poorly

  • @ArtofAvalon2
    @ArtofAvalon2 Рік тому

    Block2 will never fly It will have beenlong surpassed by Starship

    • @DavidWillisSLS
      @DavidWillisSLS  Рік тому +2

      Block 2 will fly, because there aren’t enough shuttle boosters for block 1b to fly forever