Flight plan and flight test results of experimental SST vehicle NEXST-1

ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006

Volumn 5, Issue , 2006, Pages 3305-3312

  Fujiwara, Takeshi ^a   Hirako, Keiichi ^a   Ohnuki, Takeshi ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Automatic control; Experimental airplane; Flight test; SST; Supersonic transport

Indexed keywords

AUTOMATION; ROCKETS; SPACE RESEARCH; TRANSPORT AIRCRAFT;

EXPERIMENTAL AIRPLANE; FLIGHT PLANS; FLIGHT TEST; JAPAN AEROSPACE EXPLORATION AGENCY; MAJOR EVENTS; SST; SUPERSONIC FLIGHTS; SUPERSONIC TRANSPORT; TEST RANGE; TRANSPORT PROJECTS;

SUPERSONIC AIRCRAFT;

EID: 84896937692     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Kwak D.-Y, Yoshida K, Ishikawa H, and Noguchi M. Flight Test Measurements of Surface Pressure on Unmanned Scaled Supersonic Experimental Airplane. Proc 24th AIAA Applied Aerodynamics Conference, 2006. (AIAA Paper 2006-3483).
2. Ohnuki T, Hirako K, and Sakata K. National Experimental Supersonic Transport Project. Proc 25th Congress of ICAS, 2006. (ICAS 2006-1.4.1).
3. Sakata K. Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology - Development and Flight Test Plane for the Unmanned Scaled Supersonic Glider. Proc 40th AIAA Aerospace Sciences Meeting and Exhibit, 2002. (AIAA Paper 2002-0527).
4. Tokugawa N and Yoshida K. Transition Detection on Supersonic Natural Laminar Flow Wing in the Flight. Proc 24th AIAA Applied Aerodynamics Conference, 2006. (AIAA Paper 2006-3165).