Hyper-X research vehicle experimental aerodynamics test program overview

Journal of Spacecraft and Rockets

Volumn 38, Issue 6, 2001, Pages 828-835

  Holland, Scott D ^a   Woods, William C ^a   Engelund, Walter C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; AIRFRAMES; BOOSTERS (ROCKET); DECELERATION; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; RAMJET ENGINES; SUBSONIC AERODYNAMICS; TRAJECTORIES; WIND TUNNELS;

AIRFRAME INTEGRATED SCRAMJET PROPULSION SYSTEM; HYPER X RESEARCH VEHICLE; SCRAMJET ENGINE TEST; WIND TUNNEL TESTS;

RESEARCH AIRCRAFT;

EID: 0035518187     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3772     Document Type: Article

References (17)

1. HYPER-X: Flight validation of hypersonic airbreathing technology
2. Aerodynamic database development for the Hyper-X airfame-integrated scramjet propulsion experiments
3. Hyper-X stage separation wind-tunnel test program
4. Computational fluid dynamics prediction of Hyper-X stage separation aerodynamics
5. Integrated aeropropulsive computational fluid dynamics methodology for the Hyper-X flight experiment
6. Describing uncertainties in simple-sample experiments