Recent flight test results of the joint CIAM-NASA MACH 6.5 scramjet flight program

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 1-10

  Roudakov, Alexander S ^a   Semenov, Vyacheslav L ^a   Hicks, John W ^b  

^a CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; HYPERSONIC VEHICLES; NASA; RAMJET ENGINES; ROCKETS; SUPERSONIC AIRCRAFT; WIND TUNNELS;

ACTUAL FLIGHT CONDITIONS; DUAL-MODE SCRAMJET; LAUNCH OPERATIONS; MAXIMUM VELOCITY; SUPERSONIC COMBUSTION; TECHNICAL DETAILS; TEST CONDITION; WIND TUNNEL TESTS;

SOFTWARE TESTING;

EID: 84983156804     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1643     Document Type: Conference Paper

References (2)

1. Roudakov, A.S., Y. Schickhman, V. Semenov, Ph. Novelli, and O. Fourt, "Flight Testing an Axisymmetric Scramjet: Russian Recent Advances," in proceedings of 44th Congress of the International Astronautical Federation, Oct. 16-22, 1993, Graz, Austria.
2. Roudakov, A., V. Semenov, V. Kopchenov, and C. McClinton, "Comparative Flowpath Analysis and Design Assessment of a Mach 6.5 Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine," AIAA 96-4571, Nov. 1996