Aerodynamic characteristic of hope-X configuration with twin vertical tails

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Tsujimoto, Takeshi ^a   Sakamoto, Yasuro ^a   Akimoto, Toshio ^a   Kouchiyama, Jiro ^a   Ishimoto, Shinji ^a   Aoki, Takeo ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AIR CUSHION VEHICLES; GROUND EFFECT; HYPERSONIC VEHICLES; REUSABILITY; VERTICAL STABILIZERS; WIND STRESS; WIND TUNNELS; WINGS;

AERODYNAMIC CHARACTERISTICS; AERODYNAMIC SHAPE; EXPERIMENTAL VEHICLE; KEY TECHNOLOGIES; REUSABLE LAUNCH VEHICLES; SUBSONIC SPEED; VERTICAL TAIL; WIND TUNNEL TESTS;

AERODYNAMIC CONFIGURATIONS;

EID: 85088346381     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1827     Document Type: Conference Paper

References (4)

1. nd Internal Symposium on Space Technology and Science, Morioka, Japan
2. 1 International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan
3. 1 International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan
4. nd International Symposium Atmospheric Reentry Vehicles and Systems, Arcachon, France