Analytical study of pre-cooled turbojet engine for TSTO Spaceplane-Reference-Cited by-同舟云学术

Analytical study of pre-cooled turbojet engine for TSTO Spaceplane

Published:2001-04-24 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Taguchi Hideyuki¹,Futamura Hisao¹,Yanagi Ryoji¹,Maita Masataka¹

Affiliation:

1. National Aerospace Lab., Chofu, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1838

Reference14 articles.

1. Escher, W. J. D. et. al. "Synerjet for Earth/Orbit Propulsion: Revisiting the 1966 NASA/Marquardt Composite (Airbreathing/Rocket) Propulsion System Study (NAS7-377),"AIAA-96-3040.

2. Lanshin, A. I. et. al. "Russian Aerospace Combined Propulsion Systems Research and Development Program ("ORYOL-2-1"): Progress Review,"AIAA-96-4494.

3. Balepin, V.V.etal, "KLIN Cycle :Combined Propulsion for Vertical Take Off Launcher," AIAA 97-2854.

4. Taguchi, H. et. al. "Conceptual Study of Pre-Cooled Air Turbojet / Rocket Engine with Scramjet (PATRES),"ISABE99-7024

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