A study on pre-cooled turbojet-scramjet-rocket combined engines-Reference-Cited by-同舟云学术

A study on pre-cooled turbojet-scramjet-rocket combined engines

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Taguchi Hideyuki¹,Yanagi Ryoji¹

Affiliation:

1. National Aerospace Lab., Chofu, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3777

Reference15 articles.

1. Engines,"AIAA-93-1944. (RBCC)

2. Air liquefaction and enrichment system propulsion in reusable launch vehicles

3. Turboramjets And Installation

4. Escher, William J. D."Fan Integrationinto the Hypersonic Combined-Cycle Engine: Background, Rationale and Candidate TechnicalApproaches," AIAA-96-2684.

5. Balepin, V. et. al. "Combined Propulsion for SSTO Rocket: From Conceptual Study to Demonstrator of Deep Cooled Turbojet," AIAA-96-4497.

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