X-33 hypersonic aerodynamic characteristics

Journal of Spacecraft and Rockets

Volumn 38, Issue 5, 2001, Pages 670-683

  Murphy, K J ^a   Nowak, R J ^a   Thompson, R A ^a   Hollis, B R ^a   Prabhu, R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATABASE SYSTEMS; LAUNCHING; REUSABLE ROCKETS; SPACE RESEARCH; SPECIFIC HEAT; SUPERSONIC AERODYNAMICS;

REUSABLE LAUNCH VEHICLES;

HYPERSONIC AERODYNAMICS;

EID: 0035439246     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3752     Document Type: Article

References (15)

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4. Langley aerothermodynamic facilities complex: Enhancements and testing capabilities
5. Overview of selected measurement techniques for aerodynamic testing in the NASA langley unitary plan wind tunnel
6. X-33 aerodynamic computations and comparisons with wind-tunnel data
7. Review of X-33 hypersonic aerodynamic and aerothermodynamic development
8. Experimental and predicted aerodynamic characteristics of a proposed Assured Crew Return Vehicle (ACRV) lifting-body configuration
9. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
10. X-38 experimental aerothermodynamics
11. X-33 hypersonic boundary layer transition