SCOPUS 정보 검색 플랫폼

Journal of Spacecraft and Rockets

Volumn 38, Issue 6, 2001, Pages 811-819

Hyper-X stage separation wind-tunnel test program

(3) Woods, William C a Holland, Scott D a DiFulvio, Michael a

a NASA LANGLEY RESEARCH CENTER (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; AIRFRAMES; BOOSTERS (ROCKET); COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; MONTE CARLO METHODS; RAMJET ENGINES; WIND TUNNELS;

ENGINE TEST POINT; HYPER X LAUNCH VEHICLE; HYPER X RESEARCH VEHICLE; STAGE SEPARATION EVENT; SUPERSONIC COMBUSTION RAMJET ENGINE; WIND TUNNEL TESTS;

RESEARCH AIRCRAFT;

EID: 0035518652 PISSN: 00224650 EISSN: 15336794 Source Type: Journal
DOI: 10.2514/2.3770 Document Type: Article

Times cited : (40)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.