Crew Surviral and Intact Abort Using Solid Rocket Boosters
32nd, Joint propulsion conference ; 1996 ; Lake Buena Vista; FL
1996-01-01
ALL
Nos 96-2540 to 96-3309 with gaps held only; See also 6237.630 nos 164 and 166 1996 for further separate papers and 6369.400F for papers on fiche (up to 3309)
Aufsatz (Konferenz)
Englisch
AIAA , ASME , SAE , ASEE , propulsion
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Intact Abort Technology Requirements
NTIS | 1970
|Thrust Oscillations in Large Solid Rocket Boosters
AIAA | 2008
|Intact abort technology requirements
NTRS | 1970
|Technology for low cost solid rocket boosters
NTRS | 1971
|