Hyper-X Flight Engine ground testing for X-43 flight risk reduction

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

Volumn , Issue , 2001, Pages

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

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; ENGINES; HYPERSONIC VEHICLES; NASA; SOFTWARE TESTING; STRUCTURAL FRAMES;

AIRFRAME INTEGRATED SCRAMJET ENGINES; AIRFRAME STRUCTURES; ENGINE PERFORMANCE; FLIGHT CONDITIONS; HIGH TEMPERATURE; RESEARCH VEHICLES; RISK REDUCTIONS; SCRAMJET ENGINES;

RAMJET ENGINES;

EID: 85085404642     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1809     Document Type: Conference Paper

References (9)

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. 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.
4. Huebner, L. D.; Rock, K. E.; Witte, D. W.; Ruf, E. G.; and Andrews, Jr., E. H.: Hyper-X Engine Testing in the NASA Langley 8-Foot High Temperature Tunnel. AIAA 2000-3605, July 2000.
5. Hodge, J. S.; and Harvin, S. E: Test Capabilities and Recent Experiences in the NASA Langley 8-Foot High Temperature Tunnel. AIAA 2000-2646, June 2000.
6. Berry, S. A.; Auslender, A. H., Dilley, A. D.; and Calleja, J. E: Hypersonic Boundary-Layer Trip Development for Hyper-X. AIAA 2000-4012, August 2000.
7. Daryabeigi, K.; and Huebner, L. D.: Heating Rate Measurements on Hyper-X Wing Gap. Proposed NASA Technical Memorandum, Draft completed December 2000.
8. 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 Research Vehicle. ISABE 99-7215, September 1999.
9. Cockrell, Jr., C. E.; Engelund, W. C; Bittner, R. D.; Dilley, A. D.; and Jentink, T. N.: Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment. AIAA 2000-4010, August 2000.