Influences of particle size and content of HMX on burning characteristics of HMX-based propellant
-
Published:2013-06
Issue:1
Volume:27
Page:209-215
-
ISSN:1270-9638
-
Container-title:Aerospace Science and Technology
-
language:en
-
Short-container-title:Aerospace Science and Technology
Author:
Naya Tomoki,Kohga Makoto
Subject
Aerospace Engineering
Reference23 articles.
1. Burning rate of solid propellant ingredients, Part 1: Pressure and initial temperature effects;Atwood;J. Propul. Power,1999
2. Burning rate of solid propellant ingredients, Part 2: Determination of burning rate temperature sensitivity;Atwood;J. Propul. Power,1999
3. M. Beckstead, Modeling calculations for HMX composite propellants, in: AIAA, ASME, SAE, and ASEE Joint Propulsion Conference, 1980.
4. Solid propellant combustion mechanisms and flame structure;Beckstead;Pure Appl. Chem.,1993
5. Modeling calculations for HMX composite propellants;Beckstead;AIAA Journal,1982
Cited by
38 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