Theory of hypergolic ignition of solid propellants-Reference-Cited by-同舟云学术

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Theory of hypergolic ignition of solid propellants

Published:1963-08-16 Issue: Volume: Page:
ISSN:
Container-title:Heterogeneous Combustion Conference
language:
Short-container-title:

Author:

ANDERSON R.¹,BROWN R.¹,EBELING R.¹

Affiliation:

1. UNITED AIRCRAFT CORP., UNITED TECHNOLOGY CENTER, SUNNYVALE, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1963-514

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors;International Journal of Aerospace Engineering;2019-12-31

2. Hypergolicity of Mixed Oxides of Nitrogen with Solid Fuels for Hybrid Rocket Application;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

3. Numerical Modeling and Studies of Ignition Transients in End-Burning-Grain Solid Rocket Motors;Journal of Propulsion and Power;2016-11

4. Ignition of solid propellants;Journal of Applied Mechanics and Technical Physics;1972

5. THE MONTE CARLO DYNAMIC ANALYSIS FOR LUNAR MODULE LANDING LOADS;11th Structures, Structural Dynamics, and Materials Conference;1970-04-22

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