Investigation of pyrotechnic MTV compositions for rocket motor igniters-Reference-Cited by-同舟云学术

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Investigation of pyrotechnic MTV compositions for rocket motor igniters

Published:1982-06-21 Issue: Volume: Page:
ISSN:
Container-title:18th Joint Propulsion Conference
language:
Short-container-title:

Author:

PERETZ A.¹

Affiliation:

1. Raphael Armament Development Authority, Propulsion Dept., Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1189

Reference11 articles.

1. Parametric Study of the Effect of Acceleration on the Burning Rate of Metalized Solid Propellants," AIM Paper 81-1584,July 1981. 1. Keller, R.B., Jr. (ed.),"Solid Rocket Motor

2. tions and Applications," AIM Paper 72-1195, November-December 1972. 4. Crosby, R., Mullenix G.C., and Swenson, I.

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3. Boron and Polytetrafluoroethylene as a Fuel Composition for Hybrid Rocket Applications;Journal of Propulsion and Power;2015-01

4. Combustion of Boron and Fluorocarbon Solid Fuels in a Hybrid Rocket;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

5. Combustion;Metal-Fluorocarbon Based Energetic Materials;2011-12-16

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