Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered single-stage-to-orbit (SSTO) vehicle-Reference-Cited by-同舟云学术

Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered single-stage-to-orbit (SSTO) vehicle

Published:1989-07-12 Issue: Volume: Page:
ISSN:
Container-title:25th Joint Propulsion Conference
language:
Short-container-title:

Author:

FOSTER RICHARD¹,ESCHER WILLIAM²,ROBINSON JOHN³

Affiliation:

1. Astronautics Corporation of America, Madison, WI

2. NASA, Washington, DC

3. Martin Marietta Corp., Astronautics Group, Denver, CO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2294

Reference20 articles.

1. Foster, R. W., Escher, W. I. D., and Robinson, I.W. "Air Augmented Rocket Propulsion Concepts", USAF Astronautics LaboratoryReport AFAL-TR-88-004, April 1988

2. Mossman, E.A., Rozycki, R.C., and Holle, G.F. "A Summary of Research on a Nozzle-Ejector System", Martin Denver Research Report R-3.31, October 1960

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