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ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
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Topic: ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section (Read 2645 times)
jongoff
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ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
«
on:
09/24/2008 05:30 pm »
I'm not sure whether this is in the right part of the forum or not, but I wanted to mention that there was an interesting Space 2008 paper presented by some friends of mine at ULA. It discusses using mid-air recovery techniques that they've been developing with Vertigo, Inc to reuse the RD-180/propulsion section of the Atlas-V.
I have a link to the paper and a review on Selenian Boondocks:
http://selenianboondocks.com/2008/09/partial-rocket-reuse-using-mid-air-recovery-a-review/
~Jon
PS If this should go in the US Launchers, Advanced Concepts, or Alternative Architectures sections, could someone move the thread?
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pippin
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Re: ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
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Reply #1 on:
09/24/2008 05:53 pm »
Interesting paper.
One thing that comes to my mind, though, is whether that flight rate issue is really one.
I mean, 10-15 engines a year... what is Atlas' flight rate right now? Or Atlas+Delta IV combined flight rate?
OK, if you think about an Atlas Heavy as an Ares replacement... but other than that I don't buy this rationale.
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Last Edit: 09/24/2008 05:53 pm by pippin
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josh_simonson
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Re: ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
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Reply #2 on:
09/24/2008 06:19 pm »
Looks mostly like FUD to make the Russians doubt their pricing power to me...
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pippin
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Re: ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
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Reply #3 on:
09/24/2008 06:26 pm »
another thing: Regarding the part about the upper stage recovery:
Does anybody know what happened to the project to recover Fregat upper stages? IIRC that was even flown once?
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jongoff
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Re: ULA Paper on Mid-Air Recovery for the Atlas-V First Stage Propulsion Section
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Reply #4 on:
09/24/2008 06:50 pm »
Pippin, Josh,
Yeah, as I said in the review, at current flight rate this isn't economically justified. Which is why they're mostly doing only the proof-of-concept work with IRAD. It's mostly to show that there's a way that they could up the flight rate substantially (while decreasing the per-flight cost substantially) if they needed to replace Ares-1, or if Bigelow gave them a contract. It's not something that I think they're actually going to field at current flight rates. Now, if they were able to sign a big contract with someone for enough flights, they could justify spending the money to finish fielding the capability.
And yes, it's a way of letting the Russians know that they don't necessarily have ULA over the barrel for the RD-180s.
As for Fregat reuse, I don't know if that was ever pursued much further. Lots of people have discussed the idea, but it still needs some work.
~Jon
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