Analytical study of pre-cooled turbojet engine for TSTO spaceplane

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

Volumn , Issue , 2001, Pages

  Taguchi, Hideyuki ^a   Futamura, Hisao ^a   Yanagi, Ryoji ^a   Maita, Masataka ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 29044444643     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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6. Taguchi, H. et al., Conceptual Study of Pre-Cooled Air Turbojet/Rocket Engine with Scramjet (PATRES), ISABE 99-7024
7. Taguchi, H. and Yanagi, R., A Study on Pre-Cooled Turbojet - Scramjet - Rocket Combined Engines, AIAA-98-3777.
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10. Kanda, T. and Kudo, K, Payload to Low Earth Orbit by Aerospace Plane with Scramjet Engine, AIAA J. Propulsion, Vol. 13, No. 1, pp. 164-166
11. Harloff, G. J. and Berkowitz, B. M., HASA-Hypersonic Aerospace Sizing Analysis for the Preliminary Design of Aerospace Vehicles, NASA CR-182226, 1988.
12. th Conference on Aerospace Propulsion (Japanese), pp.276-281, 1998