Shock initiation of a heated ammonium perchlorate-based propellant-Reference-Cited by-同舟云学术

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Shock initiation of a heated ammonium perchlorate-based propellant

Published:1996-04 Issue:1-2 Volume:105 Page:123-131
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Tarver Craig M,Urtiew Paul A,Tao William C

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference32 articles.

1. Prediction of the Critical Diameter of Composite Propellants

2. Hoffman, D.M., Lawrence Livermore National Laboratory, private communication, 1994.

3. Garcia, F., Lawrence Livermore National Laboratory, private communication, 1994.

4. Eighth Symposium (International) on Detonation;Tarver,1985

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1. Effects of Thermal Damage on Impact Response Characteristics of High-Energy Propellants;Polymers;2024-03-08

2. Diversity in synthetic perchlorate anion receptors: Challenges and opportunities;Journal of Molecular Structure;2023-11

3. Thermochemical release mechanisms and circumferential initiation affecting detonation in an aluminized explosive;Journal of Energetic Materials;2022-08-24

4. Enhanced decomposition of laminated ammonium perchlorate composite;Scientific Reports;2021-11-19

5. Analysis on damage characteristics and detonation performance of solid rocket engine charge subjected to jet;Defence Technology;2021-09

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