Development of a class 1.3 minimum smoke propellant-Reference-Cited by-同舟云学术

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Development of a class 1.3 minimum smoke propellant

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

BIVIN R.¹,JOHNSON J.¹,MARKOVITCH I.¹,MEHROTRA ASHOK¹

Affiliation:

1. Olin/Rocket Research Co., Marion, IL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3724

Reference4 articles.

1. Meeting at Indianapolis, IN, W February 1992. 2 Baseline Formulation: AN=63.0,

2. 9 (+56)(-60) 05% A-1120-0.25%

3. Formulation: ORP-2 -7.5% B"N/TMETN -27.2% MNA-0.5% CB-0.5% A-1120-0.25%

Cited by 3 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. Combustion mechanism of nitro ester binders with nitramines;Combustion, Explosion, and Shock Waves;2012-03

2. An Advanced GAP/AN/TAGN Propellant. Part I: Ballistic Properties;Propellants, Explosives, Pyrotechnics;2007-04

3. Characteristic Properties of AN/GAP-Propellants;Propellants, Explosives, Pyrotechnics;1996-06

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