Comprehensive Study of AP Particle Size and Loading Effects on the Burning Rates of Composite AP/HTPB Propellants-Reference-Cited by-同舟云学术

Comprehensive Study of AP Particle Size and Loading Effects on the Burning Rates of Composite AP/HTPB Propellants

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 Joint Propulsion Conference
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Author:

Thomas James C.¹,Morrow Gordon R.¹,Dillier Catherine A.¹,Petersen Eric L.¹

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4874

Reference30 articles.

1. Bastress, E. K. "Modification of the Burning Rates of Ammonium Perchlorate Solid Propellants by Particle Size Control," Ph.D. Dissertation,Department of Aeronautical Engineering, Princeton University, Princeton, NJ,1961.

2. Experimental and theoretical study of the effects of pressure and crossflow velocity on composite propellant burning rate

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