A preliminary design code for hybrid propellant rockets-Reference-Cited by-同舟云学术

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A preliminary design code for hybrid propellant rockets

Published:1994-01-10 Issue: Volume: Page:
ISSN:
Container-title:32nd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Werthman W.¹,Schroeder Christine¹

Affiliation:

1. Purdue Univ., West Lafayette, IN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-6

Reference9 articles.

1. AIAAJSAWASMEJASEE,July 6-8,1992.

2. Heister,S.D. "AComputerCodeforSolidRocket MotorDesign(SRMDESVersion 2.0)Technical DescriptionandUser'sManual",MR-0900(9975)-3, 15June 1990,TbeAerospaceCorporation,El Segundo,Calif.

3. Sutton,G.P. "TurbopumpFeed System",Ks&t p, JohnWiley& Sons,Inc., New York,1992,pp.327-344.

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