https://www.stokespace.com/nova/
- 3,000 kg to LEO (100% reusable)
- 7,000 kg to LEO (max payload)
- 2,500 kg to GTO
- 1,250 kg to TLI
- 800 kg to C3 = 0
Thanks!Wonderful article; really excited to see where this company can take their design and see what they can do. Seems a very innovative design if they can pull it off.
Also, there's a typo on the hop test picture notes. Says "Stoke Space’s Hopper 2 takes to the skies in September 2003 in Moses Lake, Washington." The article section that follows has the correct year (2023).
They initially raised $9.1 million. Then they did subsequent raises from there.Surely you have a type here
"raising $9.1 million"
I can't believe they conducted a 2 year environmental assessment and rebuilt an entire launch complex on $9M.
$9.1M seedSurely you have a type here
"raising $9.1 million"
I can't believe they conducted a 2 year environmental assessment and rebuilt an entire launch complex on $9M.
Well, head over to the latest Rocket Report for your morning rocket-related humor!Damn. I just woke up and my mind read 'Stoke' as 'Pythom' and now I'm sad; I needed a giggle.
So what do people think?
Did Stoke justify we indeed do need a 151st space company?
I think the article ends with a "No. Not yet."
So what do people think?
Did Stoke justify we indeed do need a 151st space company?
I think the article ends with a "No. Not yet."
I guess that is kind of an answer, isn't it?
Speaking of small launch companies, whatever happened with those guys who were planning to put a rocket on a centrifuge and get it up to like 10k rpms and then have it shoot up halfway to space just from the rotational energy? Stoke might have some fun new engine types but those weirdos were trying something way more fun.
until I realized this is a metaphor, and not the Oort Cloud.Stoke Space isn’t shooting for the Moon. It’s shooting for something 1 million times further.
Pretty sure that's gravel from the ground in front of the test cell being carried along with the air entrained by the exhaust plume.What's with all the particles in the exhaust?
At a guess, because it would be brackish swamp water with lots of dissolved limestone and all of those contaminants would be sprayed onto your rocket and ground service equipmentWhy not use the high water table to their advantage, letting it partially fill the flame diverter and using that additional water to absorb the energy before it's blown out of the trench? This could make water deluge systems smaller and simpler.
It's not just a matter of having a puddle of water at the bottom. You need to feed in a constant flow to replace the water that boils/flies away under the heat and pressure of the rocket exhaust. That requires a complex plumbing setup, which you don't want sitting in a pool of salty water.Why not use the high water table to their advantage, letting it partially fill the flame diverter and using that additional water to absorb the energy before it's blown out of the trench? This could make water deluge systems smaller and simpler.
I don’t know the right answer, but I imagine environmental concerns as well as contaminants (e.g. salt)Why not use the high water table to their advantage, letting it partially fill the flame diverter and using that additional water to absorb the energy before it's blown out of the trench? This could make water deluge systems smaller and simpler.
Second stage re-use without a tile-based heatshield, that doesn't require massive GSE like Starship (so could theoretically land on a concrete slab of sufficient heat resistance anywhere on earth)?There was a lot of detail in this article - but I'm still wondering what Stoke offers that is new? SpaceX reuses and Raptor is full-flow. So.. what's new? A somewhat different engine design and no heatshield? A little more reusable?
I mean, if you wanted to start an Amazon competitor today and your pitch was "well we will make it a little easier to buy stuff"... that's what Wayfair is trying. How's that working out for them? I guess they're alive.
Who really thinks that if Stoke proves out some better design wrinkles, SpaceX won't be using them in about a minute?
We need real alternatives, not a Tiktok vs Facebook. I was bummed when Spinlaunch proved to be not-so-real. A Beanstalk is way off. We need something new, or SpaceX is frankly gonna be good enough for this bit.
They are pursuing a different approach to second stage reusability. Instead of insulating tiles, they will be using hydrogen to actively cool a metallic heatshield. Their upper stage engine uses an expander cycle, so they can push hydrogen through the heatshield using the same pump (in this case, the heat for the expansion comes from the heatshield, rather than the combustion chamber).There was a lot of detail in this article - but I'm still wondering what Stoke offers that is new? SpaceX reuses and Raptor is full-flow. So.. what's new? A somewhat different engine design and no heatshield? A little more reusable?
I mean, if you wanted to start an Amazon competitor today and your pitch was "well we will make it a little easier to buy stuff"... that's what Wayfair is trying. How's that working out for them? I guess they're alive.
Who really thinks that if Stoke proves out some better design wrinkles, SpaceX won't be using them in about a minute? Their positional and vertical advantages at this point are crushing. Pretty much their own downside risk is Musk's personality/public image.
We need real alternatives, not a Tiktok vs Facebook. I was bummed when Spinlaunch proved to be not-so-real. A Beanstalk is way off. We need something new, or SpaceX is frankly gonna be good enough for this bit.
Think of him as the 'Anti-Bechtel'.I think a deep-dive back story of Jonathan Lund with the launch site design/construction and the inherent problems would be a fascinating read.
Footage of their tests should really be soundtracked with the 'Monty Python' theme.Speaking of small launch companies, whatever happened with those guys who were planning to put a rocket on a centrifuge and get it up to like 10k rpms and then have it shoot up halfway to space just from the rotational energy? Stoke might have some fun new engine types but those weirdos were trying something way more fun.
Stoke's solution may not scale to the sizes SpaceX want. As their upper stage gets bigger they start to run into the square-cube problem - the mass of the stage goes up faster than the width of the heat-shield, which means the shield performance has to increase to match. And eventually you won't be able to pump enough hydrogen through the shield to cool it down enough.What I mean is, this is small stuff. If this works out massively, the most logical thing for SpaceX to do, assuming they couldn't quickly duplicate the tech (which is an assumption I wouldn't bet a nickel on, given their track record), would be to buy them out. Happens literally all the time all over every tech industry. Obviously a buyout pleases the investors vs losing everything in a failure, but it's not really that interesting to the rest of the human race.
They'll be something like cost competitive, but that's not the same thing as "in this segment we crush SpaceX so everyone goes with us".
That's what a game change would look like. A cost competitive alternative.. is nice I guess. But it's evolution, not revolution.
That is half a set of wheels in SLS money.Surely you have a type here
"raising $9.1 million"
I can't believe they conducted a 2 year environmental assessment and rebuilt an entire launch complex on $9M.
Pretty sure that's gravel from the ground in front of the test cell being carried along with the air entrained by the exhaust plume.
There's no evidence of it in the photo taken inside the test cell (with a concrete floor)