Hyper-X stage separation-simulation development and results

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Reubush, David E ^a   Martin, John G ^a   Robinson, Jeffrey S ^a   Bose, David M ^a   Strovers, Brian K ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Analytical Mechanics Associates   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); FLIGHT SIMULATORS; HYPERSONIC VEHICLES; MONTE CARLO METHODS; NASA; RISK ASSESSMENT;

AIR BREATHING VEHICLES; DEGREE OF FREEDOM; FLIGHT ENVIRONMENT; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; MONTE CARLO ANALYSIS; RISK OF FAILURE; STAGE SEPARATION;

SEPARATION;

EID: 85087192347     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1802     Document Type: Conference Paper

References (9)

1. Reubush, David E.: Hyper-X Stage Separation- Background and Status. AIAA 99-4818, AIAA 9th International Space Planes and Hypersonic Systems and Technologies Conf., Norfolk, VA, Nov. 1999.
2. Anon.: Using ADAMS/Solver. Users Guide, Vol. 9.0.1, 1997, Mechanical Dynamics, Inc.
3. Woods, W. C; Holland, S. D.; and DiFulvio, M.: Hyper-X Stage Separation Wind Tunnel Test Program. AIAA 2000-4008. AIAA Applied Aerodynamics Conference, Denver, CO, Aug. 2000.
4. Engelund, W. C; Holland, S. D.; Cockrell, C. E., Jr.; and Bittner, R. D.: Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments. AIAA 2000-4006. AIAA Applied Aerodynamics Conference, Denver, CO, Aug. 2000.
5. Buning, P. G. and Wong, T.: Prediction of Hyper-X Stage Separation Aerodynamics Using CFD. AIAA 2000-4009. AIAA Applied Aerodynamics Conference, Denver, CO, Aug. 2000.
6. Bowersox, R. D.: Uncertainty Analysis of the Mach 6.0 Hyper-X Free Flyer and Booster Separation Wind Tunnel Data. Hyper-X Program Office HX-703, SSD-00-07, Nov. 2000.
7. Justus, et al.: The NASA/MSFC Global Reference Atmosphere Model-1995 Version, NASA TM 4715.
8. Farrell, J. A. and Barth, M.: The Global Positioning System & Inertial Navigation, McGraw-Hill, 1999, pp. 187-240.
9. Huebner, L. D.; Rock, K. E.; Witte, D. W.; Ruf, E. G.; and Andrews, E. H., Jr.: Hyper-X Engine Testing in the NASA Langley 8-foot High Temperature Tunnel. AIAA 2000-3605. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, Jul. 2000.