Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics-Reference-Cited by-同舟云学术

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Influence of Initial Propellant Temperature on Solid Rocket Internal Ballistics

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

Greatrix David R.¹

Affiliation:

1. Ryerson University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4007

Reference22 articles.

1. Powered Flight

2. EXPERIMENTS ON NONLINEAR AXIAL COMBUSTION INSTABILITY IN SOLID PROPELLANT ROCKET MOTORS

3. Effects of Temperature Conditioned Environment on a Propellant's Pressure-Coupled Response

4. Mass Flux, kg/m2-s 0 1000 2000 3000 4000 0 1 2 3 294 K 233 K 313 K Figure3(a) Burning rateaugmentationratio

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