Experimental Investigation of Propellant Erosion-Reference-Cited by-同舟云学术

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Experimental Investigation of Propellant Erosion

Published:1960-02 Issue:2 Volume:30 Page:173-178
ISSN:1936-9972
Container-title:ARS Journal
language:en
Short-container-title:ARS Journal

Author:

MARKLUND TAGE¹,LAKE ARNE¹

Affiliation:

1. Research Institute of National Defense, Stockholm, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.5024

Reference7 articles.

1. Lenngren, C. E., Person, L. and Petersson, S. "A Method of Investigation of the Erosion of Rocket Propellants," Tech. Rep. NZP 7-55, Bofors, 1955(inSwedish).

2. Vandenkerckhove, J. "Combustion and Propulsion," Third Agard Colloquium, London, Pergamon Press, Inc., N. Y.1958, pp.423-425.

Cited by 52 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. Excessive Subsurface Heat Release As a Possible Cause of the Negative Erosion Effect during Combustion of Homogeneous Solid Propellants;Combustion, Explosion, and Shock Waves;2022-12

2. A New Erosive Burning Model of Solid Propellant Based on Heat Transfer Equilibrium at Propellant Surface;International Journal of Aerospace Engineering;2020-12-08

3. Study of Maximum Pressure Rise with Erosive Burning in Multi‐Grain Tubular Solid Propellant;Propellants, Explosives, Pyrotechnics;2020-07-16

4. Combustion characteristics of solid propellants under high-temperature dense-particle erosion conditions;Combustion and Flame;2019-06

5. Modeling of Heterogeneous Propellant Combustion: A Survey;AIAA Journal;2012-05

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