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#1
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DynaSoar in USAF service around 1967 : how does this influence NASA shuttle in 1969 ?
Title says all!
Suppose that DynaSoar survived Mc Namara in 1963 and entered USAF service around 1967. How does this influence the Shuttle, which program started in summer 1969 ? NASA has negative feelings towards spaceplanes after seeing USAF experience maybe ? Discuss... |
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#2
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As I understand the way things went, Nixon had a choice to have NASa pursue either a shutte program, or a Mars program. If the USAF was already doing what amounted to a shuttle, I would think NASA goes ahead with a MArs program. Probabkly landing a manned Mars mission sometime in the 1980's.
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USS Galileo Galilei, NCC-8888 Prima Inter Pares |
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#3
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Thank you.
to me there's various scenarios in the case USAF put Dynasoar in service. Or NASA buy two of them as reusable spaceplane testbed and X-15 follow-on , only to discover the concept is not worth the price. Or USAF face problems similar to the current Shuttle (low subsystem reliability, awful maintenance costs or even some accidents in Challenger-style) and as a consequence NASA stay away from the concept. Then USAF decide that DynaSoar is a white elephant but still has faith in the spaceplane concept. So they try to build a cheaper, more reliable machine in the 70's. Contract goes to Rockwell, thus replacing OTL Shuttle. |
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#4
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Dyna Soar had wild life until was chanceld by that damm Mc Namara
First a Orbital Bomber then X-plane at last Allround Shuttle: reconnaissance, bombing, shoot down Enermy Spysat or bring 4 astronaut to USAF space station. the Dyna Soar main problem is internal structure This was designed to compensate for thermal expansion of the hot structure during re-entry the sovjet copy it for Buran space Shuttle who almost brake apart durnig reentry, because over heat. USAF and Boenig had found that out in 1966 January 1. with first unmanned flight of Dyna Soar. this delay the Program for modifcation of internal structure, for next Manned Flight. to 1967 until James Wayne Wood makes his first Dyna Soar space flight. to year 1969 Dyna Soar makes 10 manned flights. in same time NASA study Space Shuttle wat happen with Dyna Soar in that Time will chance the shuttle program in worst case the Shuttle look somthing like this ![]() ![]() real proposal of rockwell for Alterantive Shuttle concept. |
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#5
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#6
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To me it looks like a soap box
. Nice model to put in your bathroom! More seriously Quote:
You mean that Dynasoar would have had structure problems, burning during reentry ? ![]() |
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#7
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the truss structure of Dyna was not yet testet in real flight truss structure of Rene 41 steel. This was designed to compensate for thermal expansion of the hot structure during re-entry. more here http://www.astronautix.com/craft/dynasoar.htm |
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#8
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But of course the funding for 3. was cancelled, leaving NASA with a rather superfluous 1. and 2.... |
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#9
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the Boeing 1969 Study "Integrated Manned Interplanetary Spacecraft." need only Saturn V and Saturn IB the mission module serve as Space Station for assembly Crew ![]() you save bilions of Dollar with no Shuttle/Station developent the mission module prototype sever as Space Station for Hardware Test in orbit. |
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#10
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I wonder how much of an influence 1970s environmental-type attitudes had on the Shuttle - the obsession with making a 'reusable, recyclable' spacecraft, even though repairing it for each new mission cost more than building an entirely new capsule+cargo combination that would do the same job... |
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#11
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Something possible more weighing is what the effect of a nuclear-capable weapons system that can head for Moscow within twenty minutes of an order to launch and giving Soviet radars no more than three minutes warning does to the international situation.
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#12
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They could be recalled, though, and retargeted...for reconnaissance, well...they might offer a combination of the advantages of a spyplane and a photoreconnaissance satellite...ideally.
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Proud Member of the United Sensible Federation--Since January 19th, 2005 And as always, no offense unless otherwise indicated. |
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#13
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Agree! and you need even less for a flyby. Btw improved Saturne V (F-1A, J-2S and 4*156 inch boosters) would have had doubled the LEO payolad up to 250 metric tons. |
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#14
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Rockwell made study of Mars Fly By Mission
with only 47000 kg ! (Apollo CSM - Mission Module for 3 Men - Marsprobe) you know Robert Zubrin Mars Direct ? The first launch would deliver an unfuelled and unmanned Earth Return Vehicle (ERV) to the Martian surface After landing an on-board production plant would generate methane/oxygen propellants. (out Mars atmosphere) A second launch would deliver the four-person crew in Habitation module. Following eighteen months of extensive exploration of the surface, they would enter the ERV and return directly to Earth. The same launch vehicles and spacecraft developed for Mars Direct could also support a lunar base. Launch mass ERV 40000 kg and HM 35200 kg Saturn V 47000 kg to Moon and Mars a Nuclear variant of Mars Direct need only one launch ERV+HB are same craft After landing an on-board production plant would generate carbondioxid propellant (out Mars atmosphere) for NERVA engine and Lunar variant can use oxygen made from lunarsoil. http://www.astronautix.com/craft/marirect.htm |
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#15
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Dyna-Soar doesn't have the same flight characteristics as an ICBM, so yes, it is an element-of-surprise thing. 3 minutes as opposed to 20 minutes, even after the Soviet satellite system comes online. Quote:
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