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Space

Stoke Space Aims To Build Rapidly Reusable Rocket With a Completely Novel Design (arstechnica.com) 62

Andy Lapsa and Tom Feldman, former Blue Origin engineers and the founders of Stoke Space, are working to develop the first fully recyclable space rocket -- one that features a reusable first and second stage. Here's an excerpt from Ars Technica's exclusive report, written by Eric Berger: In the 20 months since its initial seed round of funding, Stoke has built a second-stage engine, a prototype for the second stage, turbopumps, and manufacturing facilities. It also increased its headcount to 72 people and finalized the overall design for the rocket, which has a lift capacity of 1.65 metric tons to low-Earth orbit, in fully reusable mode. Last month, the company started to test-fire its upper-stage engines at a facility in Moses Lake, Washington. The images and video show an intriguing-looking ring with 15 discrete thrusters firing for several seconds. The circular structure is 13 feet in diameter, and this novel-looking design is Stoke's answer to one of the biggest challenges of getting a second stage back from orbit.

Most commonly, a traditional rocket has an upper stage with a single engine. This second-stage rocket engine has a larger nozzle -- often bell-shaped -- to optimize the flow of engine exhaust in a vacuum. Because all parts of a rocket are designed to be as light as possible, such extended nozzles are often fairly fragile because they're only exposed above Earth's atmosphere. So one problem with getting an upper stage back from Earth, especially if you want to use the engine to control and slow its descent, is protecting this large nozzle. One way to do that is to bury the engine nozzle in a large heat shield, but that would require more structure and mass, and it may not be dynamically stable. Stoke's answer was using a ring of 30 smaller thrusters. (The tests last month only employed 15 of the 30 thrusters). In a vacuum, the plumes from these nozzles are designed to merge and act as one. And during reentry, with a smaller number of smaller thrusters firing, it's easier to protect the nozzles. "What you're seeing in the photos of the test is a high-performance upper-stage engine that can operate within atmosphere at deep throttle to support vertical landing but then also perform at a higher ISP than some variants of the RL 10 engine in space," Lapsa said.

Another significant second-stage problem is protecting the whole vehicle from the super-heated atmosphere during reentry. NASA's Space Shuttle accomplished this with brittle thermal tiles, but these required 30,000 employee hours to inspect, test, and refurbish between flights. SpaceX is using a different type of ceramic tile, designed to be more reusable, for Starship. Given Stoke's background in rocket engines, Lapsa said it made the most sense to try a regeneratively cooled heat shield. The vehicle's ductile metallic outer layer will be lined with small cavities to flow propellant through the material to keep it cool during reentry. The second stage, therefore, will return to Earth somewhat like a space capsule -- base first, with the regeneratively cooled heat shield.

Stoke Space has a very long road ahead of it to reach space. Engine tests are an important step, but they're only the first step of many. Next up for the company is "hop" tests with a full-scale version of the second stage at the Moses Lake facility in central Washington. This prototype won't have a fairing as it would during launch, but it will still stand 19 feet tall. Initially, the tests will be low-altitude, probably measured in hundreds of feet. If there's an engineering need to go higher, the company will consider that, Lapsa said. But for now, the goal is to prove the capability to control the rocket during ascent and descent and make a soft landing. This is a shockingly difficult guidance, navigation, and control problem, especially with a novel system of distributed thrusters. "This is kind of a final proof point of this architecture," Lapsa said. "It is new. It's different. It's weird. It's original. There were a lot of questions that we had about how this thing is going to work. But we've already mitigated a lot of risk." If Stoke can manage to land the upper stage, it can move ahead with the first stage and start to turn the yet-unnamed rocket into an orbital vehicle. It sounds easy, but it's not...

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Stoke Space Aims To Build Rapidly Reusable Rocket With a Completely Novel Design

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  • by pahles ( 701275 ) on Tuesday October 11, 2022 @03:51AM (#62955549)

    working to develop the first fully recyclable space rocket

    What about those other companies that have been developing a fully recyclable space rocket for some time now? How come this one should be called 'first'?

    • Re:First? (Score:5, Informative)

      by idji ( 984038 ) on Tuesday October 11, 2022 @04:32AM (#62955605)
      because NOONE has a fully reusable orbital class rocket. Starship from SpaceX is the closest... Noone has a reusable second stage, and this idea might just work.
      • by pahles ( 701275 )
        Still, the word 'first' does not appear in the original article in reference to a fully reusable space rocket.

        SpaceX has done the same already: first develop a second stage that can land and be reused, then develop a first stage that can land and be reused, then integrate them in a fully reusable rocket. So the word 'first' is out of place. I'm not saying SpaceX was first, but Stoke Space certainly isn't.
        • It says first fully reusable space rocket... Which it would be.

          SpaceX does not re-use its second stage.
          • Who gets to claim the title "first" depends on who actually launches their rocket and completely recovers it first.
            SpaceX has been working on their fully-recoverable Starship for a lot longer than Stoke has been working on theirs; whether Stoke can catch up to SpaceX, let alone overtake them, remains to be seen.

            • Doesn't matter who has been working on it longer.
              Neither of them have completed, therefor neither is first.
              Both aim to be first.

              It is appropriate to use the following verbiage to describe both parties:
              They are both working on the first fully reusable rocket.
          • by pahles ( 701275 )
            Not for Falcon, but Starship is intented to be fully reusable.
            • I understand that, but it is not.

              One day it will be. If these guys are first, they will have the first. If SpaceX is first (seems most likely to me) then they will be first.

              Right now, first is open for grabs, as there are no fully reusable rockets.
              • by pahles ( 701275 )

                I understand that, but it is not.

                It is. It is intended to be. Like I said.

                Right now, first is open for grabs, as there are no fully reusable rockets.

                That was the intent of my first post. Like I said.

                • It is. It is intended to be. Like I said.

                  Intended to be does not matter.
                  It is not.
                  This distinction is important, because it means the title of first is no one's, and the status of "developing the first" is anyone working on one.

                  That was the intent of my first post. Like I said.

                  And I'm explaining why.
                  This article is about one such company.
                  Why does this one get to be called first? Because they all are developing the what they hope will be the first reusable rocket.
                  Whichever of them succeeds shall be the first to have done so.

                  Your complaint is odd, is all. It did not say the first to develop,

        • I think you're a bit backwards on SpaceX.

          The Falcon 9 booster (first stage) is reusable. The second stage is not, and they abandoned any attempt to make it so in favor of developing Starship.

          The Dragon capsules can be re-used, but those are the payload, not the second stage.

          If you're instead thinking of Starship (which at present is not even a usable system, much less reusable), I think its more accurate to say both stages are being developed simultaneously, with second stage style prototypes being actuall

      • by v1 ( 525388 )

        First stage reusability is comparatively simple. The main purpose of it is to get altitude, so you just need to fall back down and have enough fuel for a suicide burn at the landing. Second stage boosters are what get you up to orbital velocity. The space shuttle de-orbited by doing a dozen large wide "s-turns" in the upper atmosphere, gradually shedding velocity by carefully cooking their belly of thermal tiles. Musk's starship looks like it's going to just try a similar idea without the banking turns,

        • by shmlco ( 594907 )

          Umm.... technically the Shuttle began a deorbit by firing its OMS thrusters...

          • by v1 ( 525388 )

            Those only accounted for a small fraction of their orbital velocity. Just enough to sink down into a higher density of atmosphere that the shuttle could being the process of de-orbiting without having to wait a long time.

            Not mine, but a good explanation;

            A shuttle deorbited by facing backwards, then firing its OMS thrusters long enough to slow down about 175mph while on the other side of the planet from the runway. (At either KSC or Edwards.) That doesn't sound like much, since it was going 17,500mph, but i

        • Just above the "Hop Tests Next" section:

          Given Stoke's background in rocket engines, Lapsa said it made the most sense to try a regeneratively cooled heat shield. The vehicle's ductile metallic outer layer will be lined with small cavities to flow propellant through the material to keep it cool during reentry. The second stage, therefore, will return to Earth somewhat like a space capsule—base first, with the regeneratively cooled heat shield.

          A couple paragraphs above that they say

          And during reentry, with a smaller number of smaller thrusters firing, it's easier to protect the nozzles.

          So it sounds to me like they plan to come in engines-first like a Falcon 9 booster, only with a regenerative heat shield around the engines to handle the much higher reentry temperatures, and the engines firing to protect their nozzles.

          I assume the first photo here: https://www.stokespace.com/abo... [stokespace.com] is their second stage - it looks like an elongated reentry capsule that's mostly fuel tanks, so that tracks. Sadly they don't seem

    • by sjames ( 1099 )

      TFA says they aspire to be the first. So do the others you mention. Which one will achieve it's aspiration and actually BE the first remains to be seen.

  • by bradley13 ( 1118935 ) on Tuesday October 11, 2022 @04:15AM (#62955585) Homepage

    I've read about them elsewhere. They definitely have the right vision: Build a complete rocket (first and second stages) to be re-usable and failure tolerant. If you have a ring of engines, as they do on their second stage, you can lose more than one of them and still recover the stage.

    They ultimately dream of a rocket that can make daily trips to space. That's a long ways away, but getting a fully recoverable second stage is an important step.

  • by Opportunist ( 166417 ) on Tuesday October 11, 2022 @04:49AM (#62955621)

    Since rockets are notoriously prone to exploding, all they really do is give "vaporware" a totally new (but fairly exciting) meaning.

  • if I rotate my notebook 180 degrees.
    It also doesn't seem like much thrust with these orange flames.
    Just compare it with a SpaceX Raptor engine :
    https://www.youtube.com/watch?... [youtube.com]

    But I guess early investors get free perks like a nice baseball cap or flamethrower.

    • Do they mention what propellant their using?

      Kerosene (aka traditional jet/rocket fuel when more refined) tends to burn orange, while natural gas (aka methane when more refined) tends to burns more blue.

      I don't think the color has much to do with the efficiency of the engine.

      As for thrust - they're looking at using several small engines rather than the traditional one big one on the second stage, or Starship's three. Their second stage is also tiny - looks like it'd fit *sideways* in Starship's payload bay.

  • Serious question for any Captains out there. To me the exhaust looked more like campfire that rocket: too yellow, some green(engine rich), too turbulent to have a meaningful thrust. Can someone knowledgeable explain this?
    • I suspect it's due to some combination of
      - Not burning methane (which has a bluish flame we've all gotten used to with Starship tests)
      - Being the "dirty" flames near ignition, which are generally fuel-rich with lots of backwash from surrounding obstructions, and tend to be far more dramatically photogenic.

      Note: I have no idea what fuel they're actually using. Anyone?

      There's no Mach diamonds in the photo, so I think it's safe to say that either the engines are not working at steady-state, or the backwash fr

  • It sounds easy, but it's not...

    It's literally rocket science.

    • It's not rocket science! ...okay, well it IS rocket science, but it's not HARD.

    • by quenda ( 644621 )

      It sounds easy, but it's not...

      It's literally rocket science.

      Yeah. Hard ... but not exactly brain surgery.

  • by marcle ( 1575627 ) on Tuesday October 11, 2022 @11:21AM (#62956579)

    Eric Berger is a great space journalist, but even better is the comments section of his articles. There's a bunch of actual rocket scientists on there vigorously debating the subject at hand.

    • We used to have those on Slashdot. I remember those days. But then the constant politics posts and social justice activism drove them off. Today there are about 50 people who post regularly and who dominate conversations and bully new users off the site. It's sad, honestly.
      • You are one of the ills you describe.
        • Thinkers prefer to have the contempt of the SJWs rather than be controlled by them. Because they're worthless people. It's about time they didn't get their way for once.
      • by nomadic ( 141991 )

        "We used to have those on Slashdot. I remember those days."
        No you don't because it's always been mostly arguing about politics and culture. Back then it was mostly antisocial libertarians driving the conversation.

        "But then the constant politics posts and social justice activism drove them off"
        The fact that Slashdot has not significantly changed in 20+ years despite the rise of competitors is what drives people off.

  • Recyclable, not reusable? I think someone had a headline malfunction...

  • It seems everybody and their dog are forming rocket co's of late. While competition is good, there's not a big enough demand to accommodate so many companies, especially since it requires expensive start-up and R&D. Outer-space usage is growing, but not that much.

    Is it a case that the rich have too much money, throwing it at "cool & trendy toys"? If so, taxem!

  • and I'm not so sure about SLS either.

  • I like how this boils down to "Some guys have some plans to do stuff and think they know how they're going to do it".

  • Why would I trust an private space travel company run by qualified, experienced engineers?! Reputable private space travel companies are run by non-engineer tech bro con artists!

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