Hyper-X stage separation-background and status

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages

  Reubush, David E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC VEHICLES; NASA; WIND TUNNELS;

AIR BREATHING; FLIGHT ENVIRONMENT; GROUND TESTS; HYPER-X; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; STAGE SEPARATION; VEHICLE TECHNOLOGY;

SEPARATION;

EID: 85085845996     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4818     Document Type: Conference Paper

References (8)

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2. Hunt, J. L. and Eiswirth, E. A.: NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study. AIAA 96-. 4591, Norfolk, VA, Nov. 1996.
3. Bogar, T. J.; Alberico, J. F; Johnson, D. B; Espinosa, AM. and Lockwood, M. K.: Dual-Fuel Lifting Body Configuration Development. AIAA 96-4592, Norfolk, VA, Nov. 1996.
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5. Spradley, L. W.: Data Transfer Between SAMcfd and NASTRAN. Phase III Final Report, SBIR NASl-97107, ResearchSouth Inc., Feb. 1998.
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7. Jespersen, D. C.; Pulliam, T. H.; and Buning, P. G.: Recent Enhancements to OVERFLOW. AIAA-97-0644, Reno, NV, Jan. 1997.
8. Anon.: Using ADAMS/Solver. Users Guide, Vol. 9. 0. 1, 1997, Mechanical Dynamics, Inc.