An investigation of the acceleration induced burning rate increase of nonmetallized composite propellants-Reference-Cited by-同舟云学术

An investigation of the acceleration induced burning rate increase of nonmetallized composite propellants

Published:1970-06 Issue:6 Volume:8 Page:1062-1067
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

STURM E. J.¹,REICHENBACH R. E.¹

Affiliation:

1. Naval Postgraduate School, Monterey, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.5831

Reference9 articles.

1. An investigation of the effect of acceleration on the burning rate of composite propellants.

2. Sturm, E. J. "A Study of the Burning Rates of Composite Solid Propellants in Acceleration Fields," Ph.D. thesis, AD832206,March 1968, Naval Postgraduate School, Monterey,Calif.

3. Summerfield, M. et al. "Burning Mechanism of Ammonium Perchlorate Propellants/' ARS Progress in Astronautics and Rocketry: Solid Propellant Rocket Research, Vol.1, edited byM. Summerfield, Academic Press, New York, 1960, pp.142-182.

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