Author Topic: Shuttle II Concepts  (Read 65084 times)

Offline RanulfC

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Re: Shuttle II Concepts
« Reply #60 on: 08/12/2013 09:46 pm »
No, far from it.
a.  NASA influenced/dictated most of the requirements and technologies that prevent X-33 from being a successful test vehicle, hence LM was right in getting a contract that limited its financial exposure.  But LM did still put in a lot of its money.  MSFC management of the project was just as much to blame.
I would not call them blameless but I recall the concepts for STS. NASA asked for a 2 stage system and all the concepts from the various industry teams were 2 stage.

You're forgetting SERV! It was an SSTO design that had NOTHING to do with what NASA "said" it wanted and everything to do with what it "wrote" it wanted :)

And it was rejected BECAUSE it wasn't exactly like the other designs being submitted :)

Randy
From The Amazing Catstronaut on the Black Arrow LV:
British physics, old chap. It's undignified to belch flames and effluvia all over the pad, what. A true gentlemen's orbital conveyance lifts itself into the air unostentatiously, with the minimum of spectacle and a modicum of grace. Not like our American cousins' launch vehicles, eh?

Offline john smith 19

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Re: Shuttle II Concepts
« Reply #61 on: 08/13/2013 07:50 pm »
You're forgetting SERV! It was an SSTO design that had NOTHING to do with what NASA "said" it wanted and everything to do with what it "wrote" it wanted :)

And it was rejected BECAUSE it wasn't exactly like the other designs being submitted :)

Reading commentaries around SERV the impression was it was unsolicited. I had not realized that it was designed to the detailed RFP.

Interesting the X33 solicitations were so different.
« Last Edit: 08/14/2013 06:45 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 Proponent

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Re: Shuttle II Concepts
« Reply #62 on: 08/14/2013 04:41 pm »
SERV (note there's no `E' at the end) had a little winged craft on it in some configurations, which looked really odd and seemed a bit pointless, since the vehicle itself was re-usable intact.  I've seen it suggested that the whole reason for the winged bit was to make it conform to the RFP.

Offline john smith 19

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Re: Shuttle II Concepts
« Reply #63 on: 08/14/2013 06:55 pm »
SERV (note there's no `E' at the end) had a little winged craft on it in some configurations, which looked really odd and seemed a bit pointless, since the vehicle itself was re-usable intact.  I've seen it suggested that the whole reason for the winged bit was to make it conform to the RFP.
Noted and changed.

SERV worked in 2 modes. Cargo and crew carriage. The cargo module met (and IRCC exceeded) the cargo spec. The winged crew module was needed either because of some black zones in the launch trajectory or because SERV as a semi ballistic vehicle did not have the cross range for the spec. Given that cross range was never used that would (in hindsight) to be an excellent trade of to get a SSTO
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 Jim

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Re: Shuttle II Concepts
« Reply #64 on: 08/14/2013 07:24 pm »

Given that cross range was never used that would (in hindsight) to be an excellent trade of to get a SSTO


No, you can't say that.  If you play that game, then manned launches from VAFB were still a requirement and AOA still a necessity.

Offline leovinus

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Re: Shuttle II Concepts
« Reply #65 on: 11/28/2025 05:38 pm »
Quote
A study by VAB from 1985-1988
Objectives:

To define requirements, options, and concepts for a second generation space shuttle to provide a basis for advanced systems and technology planning.
To provide a key element in the post-2000 space transportation system to meet national needs in the most cost-effective manner
and more
https://web.archive.org/web/19980216082838/http://vab02.larc.nasa.gov/Activities/ShuttleII/STSII.html

Offline Blackstar

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Re: Shuttle II Concepts
« Reply #66 on: 11/28/2025 07:44 pm »
When I worked on the CAIB, my group developed a policy history of all the proposals to replace shuttle up until that time. It was in the form of a Powerpoint presentation. It was pretty good, and it effectively made the case that NASA had never really thought out a shuttle replacement and stuck to that. And whenever a replacement program was canceled, they just extended the shuttle lifetime without doing a careful evaluation whether that was a good idea. I doubt I have that presentation anymore, but it probably ended up in the CAIB archival material.

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