Hyper-X program status

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

Volumn , Issue , 2001, Pages

  McClinton, Charles R ^a   Rausch, David R ^a   Sitz, Joel ^b   Reukauf, Paul ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN ACTIVITY; FLIGHT ENVIRONMENT; FLIGHT RESEARCH; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; RESEARCH VEHICLES; RISK REDUCTIONS; VEHICLE TECHNOLOGY;

HYPERSONIC VEHICLES;

EID: 85088758358     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1910     Document Type: Conference Paper

References (20)

1. Rausch, V. L.; McClinton, C. R.; and Crawford, J. L.: Hyper-X: Flight Validation of Hypersonic Airbreathing Technology. ISABE 97-7024, Sept. 7-12, 1997, Chattanooga, TN.
2. Rausch, V. L.; McClinton, C. R.; and Hicks, J. W.: NASA Scramjet Flights to Breath New Life into Hypersonics. Aerospace America, July 1997.
3. Hunt, J. L. and Eiswirth, E. A.: NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study. AIAA 96-4591, 7fh International Space Planes and Hypersonics Systems & Technology Conference, Nov. 1996.
4. Hunt, J. L. and McClinton, C. R.: Scramjet Engine/ Airframe Integration Methodology. AGARD Future Aerospace Technology Conference, Paper C35, Palaiseau, France, April 14-16,1997.
5. 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. 18th Applied Aerodynamics Conference, Aug. 14-17,2000.
6. Holland, S.D.; Woods, W.C.; and Engelund, W.C.: Hyper-X Research Vehicle (HXRV) Experimental Aerodynamic Test Program Overview. AIAA 2000-4011. 18th Applied Aerodynamics Conference, Aug. 14-17,2000.
7. Cockrell, C.E.; Engelund, W.C.; Bittner, R.D.; Dilley, A.D.; Jentink, T.N.; and Frendi, A.: Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment. AIAA 2000-4010. 18th Applied Aerodynamics Conference, Aug. 14-17, 2000.
8. 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, Jul. 2000.
9. 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.
10. Bogar, T.J.; Alberico, J.F.; Johnson, D.B.; Espinosa, A.M.; and Lockwood, M.K.: Dual-Fuel Lifting Body Configuration Development. AIAA 96-4592. Norfolk, VA, Nov., 1996.
11. Wood, W.C.; Holland, S.D.; and DiFulvio, M.: Hyper-X Stage Separation Wind Tunnel Test Program. AIAA 200-4008. AIAA 18th Applied Aerodynamics Conference, Aug. 14-17, 2000.
12. Buning, P.G. and Wong, T.: Prediction of Hyper-X Stage Separation Aerodynamics Using CFD. AIAA 2000-4009, AIAA 18th Applied Aerodynamics Conference, Aug. 14-17, 2000.
13. Reubush, D.E.: Hyper-X Stage Separation-Background and Status. AIAA 99-4818, AIAA 9th International Space Planes and Hypersonic Systems and Technologies Conference, Nov. 1-5, 1999.
14. Rogers, R. C; Capriotti, D. P.; and Guy, R. W.: Experimental Supersonic Combustion Research at NASA LaRC. AIAA 98-2506. 20th Advanced Measurement and Ground Testing Technology Conference, Jul. 1998.
15. Pegg, R. J.; Couch, B. D.; and Hunter, L. G.: Pulse Detonation Engine Air Induction System Analysis. AIAA 96-2918, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3,1996.
16. Bussing, T. R. A.; and Pappas, G.: An Introduction to Pulse Detonation Engines. AIAA 94-0263, Jan. 1994.
17. Gurijanov, E. P. and Harsha, T.: Ajax: New Directions in Hypersonic Technology. AIAA 96-4609, AIAA 7th International Space Planes and Hypersonic Systems and Technologies Conference. Nov. 18-22,1996.
18. McClinton, C.R.; Hunt, J.L.; Ricketts, R.H.; Reukauf, P.; and Peddie, C.L.: Airbreathing Hypersonic Technology, Vision Vehicles and Development Dreams, AIAA 99-4978, 9th International Space Planes and Hypersonic Conference. Nov. 1999.
19. Erdos, J. I.; Bakos, R. J.; Castrogiovanni, A.; and Rogers, R. C: Dual Mode Shock-Expansion/ Reflected-Shock Tunnel. AIAA 97-0560,35th Aerospace Sciences Meeting, Jan. 1997.
20. Hunt, J. L. and Couch, L. M.: Beyond Hyper-X, Space '98. Sixth ASCE Specialty Conference, Apr. 26-30, 1998.