CIAM/NASA Mach 6.5 scramjet flight and ground test

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages

  Voland, R T ^a,d   Auslender, A H ^a,d   Smart, M K ^b   Roudakov, A S ^c,e   Semenov, V L ^c,e   Kopchenov, V ^c,e  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Lockheed Martin Engineering Sciences   (United States)

^c CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

^d Hypersonic Airbreathing Propulsion Branch   (United States)

^e Aerospace Propulsion Department   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION; ENGINES; HYPERSONIC VEHICLES; MACH NUMBER; NASA; ROCKETS; SOFTWARE TESTING; SUPERSONIC AIRCRAFT; TEST FACILITIES; TESTING;

DUAL-MODE SCRAMJET; ENGINE PERFORMANCE; INLET PERFORMANCE; LANGLEY RESEARCH CENTERS; SCRAMJET ENGINES; SENSOR READINGS; SUBSONIC COMBUSTION; TECHNICAL ASSISTANCE;

RAMJET ENGINES;

EID: 85086055830     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4848     Document Type: Conference Paper

References (11)

1. A. Roudakov, J. Schickhman, V. Semenov, P. Novelli, O. Fourt: Flight Testing an Axisymmetrical Scramjet-Russian Recent Advances. 44th Congress of the IAF. Oct. 16-22, 1993. Graz, Austria.
2. A. Roudakov, V. Semenov and J. Hicks: Recent Flight Test Results of the Joint CIAM-NASA Mach 6. 5 Scramjet Flight Program. Presented 8th International Spaceplanes and Hypersonic Systems and Technology Conference. Norfolk, VA. AIAA Paper 98-1643, April. 1998.
3. J. R. Henry and G. Y. Anderson: Design Considerations for the Airframe-Integrated Scramjet. Presented at the 1st International Symposium on Air Breathing Engines. Marseilles, France. June 1972 (also, NASA TM X-2895, 1973).
4. V. Rausch, L. Crawford, and C. McClinton: Hyper-X Program Review. Presented at the 8th International Space Planes and Hypersonic Systems and Technology Conference. Norfolk, Virginia. April 27-30, 1998.
5. R. T. Voland, A. H. Auslender, Arid M. K. Smart: CIAM/NASA Mach 6. 5 Scramjet Flight and Ground Test Program: Analysis Results. 35th JANNAF Combustion Subcommittee/Propulsion Systems Hazards Subcommittee/& Airbreathing Propulsion Subcommittee Joint Meeting. Tucson, AZ. Dec. 7-11 1998.
6. C. McClinton, A. Roudakov, V. Semenov and V. Kopehenov: Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6. 5. 7th International Spaceplanes and Hypersonic Systems and Technology Conference. Norfolk, VA. AIAA Paper 96-4571, Nov. 1996.
7. A. Roudakov, V. Semenov, V. Kopehenov and J. Hicks: Future Flight Test Plans of an Axisymmetric Hydrogen-Fueled Scramjet Engine on the Hypersonic Flying Laboratory. 7th International Spaceplanes and Hypersonic Conference. Norfolk, VA. AIAA Paper 96-4572, Nov. 1996.
8. A. H. Auslender: An Application of Distortion Analysis to Scramjet-Combustor Performance Assessment. Scramjet Engine Performance Analysis, Evaluation, and Optimization, 1996 JANNAF Propulsion and Joint Subcommittee Meeting Scramjet Performance Workshop, Albuquerque, New Mexico.
9. M. D. Salas: Shock Fitted Method for Complicated Two-Dimensional Supersonic Flows. AIAA Journal, vol. 14, No. 5, 1976, pp 583-588.
10. S. Srinivasan and W. D. Erickson: Influence of Test-Gas Vitiation on Mixing and Combustion at Mach 7 Flight Conditions. AIAA-94-2816, June 1994.
11. Engineering Staff of Garrett Airesearch Company: Hypersonic Research Engine Project-Phase II Aerothermodynamic Integration Model Development, Final Technical Data Report. NASA Contract No. NAS 1-6666. Document No. AP-75-11133. May 19, 1975.