Rapid Solid Rocket Motor Design-Reference-Cited by-同舟云学术

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Rapid Solid Rocket Motor Design

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
Short-container-title:

Author:

Smit Gideon J.¹,Knoetze Johannes¹,Steyn Francois²,Rousseau Charle W.²,De Kock Erhardt R.¹

Affiliation:

1. Stellenbosch University

2. Rheinmetall Denel Munition

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3789

Reference10 articles.

1. 1Fleeman,E.,TacticalMissileDesign,No.ISBN-10:1-56347-782-3,AIAA,2nded.,2006.

2. 2Waliskog, H.A. and Hart, R.G., Investigation of the Drag of Blunt-Nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3, Research Memorandum L53D14a, NACA, Langley Aeronautical Laboratory, LangleyField,Virginia,June1953.

3. 3GPSutton.RocketPropulsionElements.4thed.,1975.

4. 4Davenas,A.,SolidRocketPropulsionTechnology,Pergamon,Oxford,England,1993.

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1. General Burnback Analysis for Anisotropic and Heterogeneous Solid Propellants;Journal of Propulsion and Power;2024-09

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