Author Topic: Countdown to new smallsat launchers  (Read 419772 times)

Offline TrevorMonty

Re: Countdown to new smallsat launchers
« Reply #780 on: 10/23/2020 09:43 am »
That Titanic effect helps bigger LVs on way up but is no use to lighter small LV which have higher drag losses. On plus side it allows them to do non propulsive reentry in case of Electron. Some of larger  1000-1500kg small LVs may still need reentry burn but I'm guessing lot less than likes F9.
« Last Edit: 10/23/2020 09:44 am by TrevorMonty »

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #781 on: 10/23/2020 04:37 pm »

I dunno, with the recent discussion on plastic engines, the bar may have been lowered for small engine development? Either way, the original Bricklifter/Mockingbird concept is the concept of record that nobody seems to be actively emulating, which always struck me as odd.
Perhaps you should look at the original paper on the subject. here
That's a long way from a "plastic" engine, but it suggests directions for research.

Mockingbird was a reciprocating engine concept specifically because turbo pumps are difficult at this scale and they wanted to show better than pressure fed was possible at this scale, which they did.

I meant plastic engines for an easier dev cycle allowing high physical iteration, not the final engine.

Also, due to nomenclature, I feel I should point out for those reading that the rough 5000lbs rule of thumb for turbopumps vs something else (reciprocating, specifically Whitehead envisioning a third gas driving a piston pump) is specifically referring to the difficulty of manufacturing/designing the turbine driving the compressor pump (axial or centrifugal). Which is why when Rocketlabs substituted an electric motor for the turbine, they get most of the turbopump benefits.
So it doesn't look like the bar has been lowered for small engines unless you switch to electric drive, or move to reciprocating pumps.  Small turbines remain in a particularly tricky corner of the development parameter map.  :(
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #782 on: 10/23/2020 04:47 pm »
I suspect the reason why Delta 7925 has a lower gravity loss is the higher initial acceleration from all those solids. Same with the Space Shuttle. Drag losses are mainly related to the mass to area ratio of the vehicle. A higher mass vehicle for the same area will have less drag losses, which I like to call the Titanic effect. The bigger your vehicle is, the less drag loss you will have, which is evident in the Saturn V.
Certainly possible. I think it's quite easy to view the 7925's as a 3 or even 4 stage vehicle, given the solid clusters as they fire. 

Once you realize it's not about thrust, it's about the vertical component of thrust you know the further away from the vertical, and the sooner you start to move toward the horizontal, the better.

Just as running the engine in the O:F range that puts the most of the heaviest part in the atmosphere the earliest (usually LOX) also improves acceleration. Ideally with a proportional valve gradually varying the MR during ascent.
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline Comga

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Re: Countdown to new smallsat launchers
« Reply #783 on: 10/25/2020 08:38 pm »
Can we put "Physics of small launch vehicles" into its own thread and get back on topic to "New Smallsat Launchers"?
Here's a link to the most recent version of the Original Post  edit: found it!
Would anyone care to make a current version?

edit:  It would be great if the OP contained a link to whichever post had that most recent version.
« Last Edit: 10/26/2020 03:34 am by Comga »
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline TrevorMonty

Re: Countdown to new smallsat launchers
« Reply #784 on: 10/31/2020 05:43 pm »
Jim Cantrell is back in small LV business with new company called Phantom. Must of found a Billionaire backer that wants to become Millionaire.

https://twitter.com/jamesncantrell/status/1322399546350002177?s=09
« Last Edit: 10/31/2020 05:46 pm by TrevorMonty »

Offline jstrotha0975

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Re: Countdown to new smallsat launchers
« Reply #785 on: 10/31/2020 08:02 pm »
Those who cannot learn from history are doomed to repeat it.

Offline Gliderflyer

Re: Countdown to new smallsat launchers
« Reply #786 on: 10/31/2020 08:23 pm »
Here is the website, not a lot of detail yet.

https://www.phantomspace.com/
I tried it at home

Offline niwax

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Re: Countdown to new smallsat launchers
« Reply #787 on: 10/31/2020 08:36 pm »
Those who cannot learn from history are doomed to repeat it.

And here I thought my prediction of Vector coming back from the dead was the long shot of the list.
Which booster has the most soot? SpaceX booster launch history! (discussion)

Offline Lars-J

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Re: Countdown to new smallsat launchers
« Reply #788 on: 11/01/2020 04:43 am »
Jim Cantrell is back in small LV business with new company called Phantom. Must of found a Billionaire backer that wants to become Millionaire.

https://twitter.com/jamesncantrell/status/1322399546350002177?s=09
Yikes. Any business venture with Cantrell seems ... very risky.

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #789 on: 11/01/2020 05:37 am »
Those who cannot learn from history are doomed to repeat it.
So a man walked away from SpaceX because he thought it would never turn a profit is trying to emulate them.

Again.

His investors had better hope his decision making skills and ability to tell the difference between winners and losers has improved with bankruptcy

I will wish them well.
« Last Edit: 11/01/2020 05:37 am by john smith 19 »
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline ncb1397

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Re: Countdown to new smallsat launchers
« Reply #790 on: 11/01/2020 03:00 pm »
Those who cannot learn from history are doomed to repeat it.
So a man walked away from SpaceX because he thought it would never turn a profit is trying to emulate them.

Again.

His investors had better hope his decision making skills and ability to tell the difference between winners and losers has improved with bankruptcy

I will wish them well.

I think the quote was that Elon yelled at him one too many times.

Quote
Then, less than a year later, Cantrell quit suddenly. "Elon yelled at me one too many times," he says. "I was done. And frankly, I just wasn't interested in what he was doing at the time. I really didn't think he treated this as a commercial activity." (SpaceX did not return requests for comment on Cantrell's accounts of the company's early days.)
https://www.inc.com/kevin-j-ryan/vector-building-rockets-jim-cantrell-spacex.html

Offline ringsider

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Re: Countdown to new smallsat launchers
« Reply #791 on: 11/01/2020 07:13 pm »
Quote
(SpaceX did not return requests for comment on Cantrell's accounts of the company's early days.)

That, right there, says everything you need to know.
« Last Edit: 11/01/2020 07:13 pm by ringsider »

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #792 on: 11/01/2020 08:36 pm »
I think the quote was that Elon yelled at him one too many times.

Quote
Then, less than a year later, Cantrell quit suddenly. "Elon yelled at me one too many times," he says. "I was done. And frankly, I just wasn't interested in what he was doing at the time. I really didn't think he treated this as a commercial activity." (SpaceX did not return requests for comment on Cantrell's accounts of the company's early days.)
https://www.inc.com/kevin-j-ryan/vector-building-rockets-jim-cantrell-spacex.html
Note that pronoun.
Quote
I just wasn't interested in what he was doing at the time.
Which is probably a fairly OK attitude at ULA but not going to go down well in a small startup.

Hopefully he is a bit more motivated with his 3rd attempt at a rocket launch company.

As for being able to talk for half an hour non stop my first though is "Yes, but does he say anything of importance during that half hour monologue ?"

And I've looked through the patent.  Oh $deity.  :( So unlike other engines it uses additive manufacturing in aluminum to avoid foreign object damage and minimize the number of seals.  I can barely grasp the level of innovation. Mind. Blown away.

Possibly the most innovative element of the design are bleed valves upstream of the main propellant valves which allow trapped propellants that have boiled due to heat leakage to be removed prior to ignition, easing the startup transients. Especially important if it's a pressure fed, which this seems to be. So the not-so-big dumb booster V2.0 then.  :(

Fueling a rocket with sand would also be novel (with OF3 as the oxidizer it will burn, as will asbestos  :o )

Wheather it's actually any better is a different question.  :(
« Last Edit: 11/01/2020 08:48 pm by john smith 19 »
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline Bananas_on_Mars

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Re: Countdown to new smallsat launchers
« Reply #793 on: 11/03/2020 12:48 pm »
ESA has signed contracts to support 3 german smallsat launchers HyImpulse, Isar Aerospace and Rocketfactory Augsburg to help them with their respective first launch vehicle.

https://twitter.com/esa_sts/status/1323567472541388801?s=21

https://www.esa.int/Enabling_Support/Space_Transportation/ESA_signs_first_Boost!_commercial_space_transportation_contracts

Offline Galactic Penguin SST

Re: Countdown to new smallsat launchers
« Reply #794 on: 11/07/2020 06:49 am »
The Chinese is now 2-1 to everyone else in this world for small satellite start-up LSPs reaching orbit since the 2010s IIRC....  ::)

https://twitter.com/Cosmic_Penguin/status/1324981493807026176
Astronomy & spaceflight geek penguin. In a relationship w/ Space Shuttle Discovery.

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #795 on: 11/07/2020 07:57 am »
The Chinese is now 2-1 to everyone else in this world for small satellite start-up LSPs reaching orbit since the 2010s IIRC....  ::)

https://twitter.com/Cosmic_Penguin/status/1324981493807026176
And both are solid fueled as well.

The question is of course wheather the internal Chinese market is big enough to sustain one or both of them.
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline su27k

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Re: Countdown to new smallsat launchers
« Reply #796 on: 11/07/2020 03:23 pm »
Well about that...

https://twitter.com/planet4589/status/1324999774068760577

Quote
The Gushenxing-1 is a 4 stage rocket, probably based on demilitarized solid motors from the DF-21 missile. Stage 1 and 2 are 1.4m in diameter, Stage 3 is 1.2m in dia. Stage 4 is a liquid orbit insertion stage.

https://twitter.com/planet4589/status/1325104799159881729

Quote
China's government sells demilitarized large solid rocket motors to commercial startup companies, allowing those companies to develop satellite launch vehicles rapidly

So I don't see this in anyway comparable to the rest of the world where smallsat launchers are liquid fueled and developed from scratch.

Offline Steven Pietrobon

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Re: Countdown to new smallsat launchers
« Reply #797 on: 11/08/2020 02:03 am »
So I don't see this in anyway comparable to the rest of the world where smallsat launchers are liquid fueled and developed from scratch.

The situation might be different if the US were allowed to sell its surplus military rockets to commercial companies.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline john smith 19

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Re: Countdown to new smallsat launchers
« Reply #798 on: 11/08/2020 05:37 am »
So I don't see this in anyway comparable to the rest of the world where smallsat launchers are liquid fueled and developed from scratch.
Indeed. What exactly is the "development" work they are doing here?

Changing the payload fitting from reentry vehicles to satellites? Altering some parameters in the flight computer memory so it doesn't drop on New Delhi?

I've never understood why a civilian LV provider would ever go with a solid design unless they had links into weapon systems suppliers (or in this case operators).

The supposed benefits only really benefit people who need stuff to sit around in storage for years (decades?) and be ready for nearly instant launch, which is about as far from a commercial environment as you can possibly get.
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline edzieba

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Re: Countdown to new smallsat launchers
« Reply #799 on: 11/09/2020 11:09 am »
So I don't see this in anyway comparable to the rest of the world where smallsat launchers are liquid fueled and developed from scratch.
Indeed. What exactly is the "development" work they are doing here?
- Integrating motors into stages
- Integrating stages into a rocket
- Developing the liquid upper stage (unless China has decided that selling ICMB busses on the open market is a good idea)
- Developing GN&C for the rocket
- launch operations

Barring Falcon 9, all current US launcher use engines or motors purchased from a supplier rather than developed and built in house. Even if you decide ULA doesn't count because their build their own tanks, that still eliminates Antares, Minotaur and Pegasus.

As for 'why solids'?
- Cheap availability. They've got motors, they've built launchers with them, and they've launched them. That puts them ahead of everyone other than Rocketlab in terms of actually getting to orbit.
- No inherent cost disadvantage. Current solids are expensive, because current solids are designed for high-reliability long-duration-storage applications (i.e. military use). Remove those requirements for stability and longevity, and what you have are metal tubes with a hollow polymer cast into them, where that polymer happens to be highly flammable. If you can stomach handling them, the actual motors themselves can be manufactured simply and cheaply.

 

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