Future flight test plans of an axisymmetric hydrogen-fueled scramjet engine on the hypersonic flying laboratory

Space Plane and Hypersonic Systems and Technology Conference

Volumn , Issue , 1996, Pages

  Roudakov, Alexander S ^a   Semenov, Vyacheslav L ^a   Kopchenov, Valeriy I ^a   Hickst, 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; NASA; ROCKETS; SOFTWARE TESTING; SPACECRAFT; WIND TUNNELS;

CURRENT PROJECTS; DUAL-MODE SCRAMJET; MAXIMUM VELOCITY; SCRAMJET ENGINES; SUPERSONIC COMBUSTION; TECHNICAL DETAILS; TEST CONDITION; WIND TUNNEL TESTS;

SUPERSONIC AIRCRAFT;

EID: 84983212587     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (2)

1. A. S. Y. Schickhman, V. Semenov, Ph. Novelli, and O. Fourt, “Flight Testing an Axisymmetric Scramjet: Russian Recent Advances,” 44th Congress cf 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.