Hyper-X engine testing in the NASA Langley 8-Foot High Temperature Tunnel

35th Intersociety Energy Conversion Engineering Conference and Exhibit

Volumn , Issue , 2000, Pages

  Huebner, Lawrence D ^a   Rock, Kenneth E ^a   Witte, David W ^a   Ruf, Edward G ^a   Andrews Jr , Earl H ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b FDC/NYMA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; DATABASE SYSTEMS; ENERGY CONVERSION; ENGINES; NASA; SOFTWARE TESTING; STRUCTURAL FRAMES;

AIRFRAME INTEGRATED SCRAMJET ENGINES; AIRFRAME STRUCTURES; DATABASE DEVELOPMENT; FLIGHT CONFIGURATIONS; GEOMETRIC REPRESENTATION; HIGH TEMPERATURE; RESEARCH VEHICLES; SCRAMJET ENGINES;

RAMJET ENGINES;

EID: 85088760204     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3605     Document Type: Conference Paper

References (10)

1. Rausch, V. L.; McClinton, C. R.; and Crawford, J. L.: "Hyper-X: Flight Validation of Hypersonic Airbreathing Propulsion. " ISABE 97-7024, September 1997.
2. Rausch, V. L.; McClinton, C. R.; and Sitz, J. R.: "The Hyper-X Program Overview. " ISABE 99-7213, September 1999.
3. Voland, R. T; Rock, K. E.; McClinton, C. R.; and Pinckney, S. Z.: "Hyper-X Engine Flowpath Design (U). " Presented at 1997 JANNAF CS/ PSHS/APS Joint Meetings, West Palm Beach, FL, October 27-31, 1997 (SECRET).
4. Rock, K. E.; Voland, R. T.; Rogers, R. C.; and Huebner, L. D.: NASA's Hyper-X Scramjet Engine Ground Test Program. " ISABE 99-7214, September 1999.
5. Guy, R. W.; et al.: The NASA Langley Scramjet Test Complex. " AIAA 96-3243, July 1996.
6. Huebner, L. D.; Rock, K. E.; Voland, R. T; and Wieting, A. R.: "Calibration of the Langley 8-Foot High Temperature Tunnel for Hypersonic Airbreathing Propulsion Testing. " AIAA CP-96-2197, June 1996.
7. Reubush, D. E.; Puster, R. L.; and Kelly, H. N.: "Modification to the Langley 8-Foot High Temperature Tunnel for Hypersonic Propulsion Testing. " AIAA 87-1887, June 1987.
8. Hodge, J. S.; and Harvin, S. F.: "Test Capabilities and Recent Experiences in the NASA Langley 8-Foot High Temperature Tunnel. " AIAA 2000-2646, June 2000.
9. Rock, K. E.; Nugent, M. R.; Orme, J. S.; and Calleja, J. F: "Propulsion Subsystem Control Law Development for the Hyper-X Mach 7 Flight Test. " Presented at the 1999 JANNAF CS/PSHS/ APS Joint Meetings, Cocoa Beach, FL, October 18-22, 1999.
10. Engelund, W. C.; Holland, S. D.; Cockrell, Jr., C. E.; and Bittner, R. D.: "Propulsion System Airframe Integration Issues and Aerodynamic Database Development for the Hyper-X Flight Research Vehicle. " ISABE 99-7215, September 1999.