Optimal design of two-stage-to-orbit space planes with airbreathing engines

Journal of Spacecraft and Rockets

Volumn 42, Issue 1, 2005, Pages 90-97

  Tsuchiya, Takeshi ^a,c   Mori, Takashige ^b,d  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Aeronautics ^*  (Japan)

^d Future Space Transportation Center   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOOSTERS (ROCKET); CATAPULTS (AIRCRAFT LAUNCHERS); HEAT TRANSFER; HYPERSONIC AERODYNAMICS; OPTIMIZATION; PROBLEM SOLVING; PRODUCT DESIGN; PROPELLANTS;

AIRBREATHING ENGINES; ANALYSIS PROCESS; OPTIMAL DESIGN; SPACE PLANES;

AIRCRAFT ENGINES;

EID: 14544303272     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.8012     Document Type: Article

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