Nonsteady burning of solid propellants with an external radiant heatflux - A comparison of models with experiment

Author:

SON S.1,BURR R.1,BREWSTER M.1,FINLINSON J.2,HANSON-PARR D.2

Affiliation:

1. Illinois, University, Urbana

2. U.S. Navy, Naval Weapons Center, China Lake, CA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 4 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. Critical Review of the Methods to Measure the Condensed Systems Transient Regression Rate;Eurasian Chemico-Technological Journal;2018-03-31

2. Response Functions of Propellant Burning Rate with Distributed Heat Release Due to Pyrolysis;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Laser recoil combustion response of HNF oxidizer from 1 to 6 atmospheres;33rd Joint Propulsion Conference and Exhibit;1997-07-06

4. The study of nutation instability on spinning solid propellant rockets;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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