A Promising Fuel for Variable Thrust Motor: HTPB Propellant with High Pressure Exponent
Author:
Affiliation:
1. Xi'an Modern Chemistry Research Institute Xi'an, Shaanxi 710065 China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202000009
Reference31 articles.
1. B. Austin S. Heister E. Dambach S. Meyer E. Wernimont. Variable Thrust Multiple Start Hybrid Motor Solutions for Missile and Space Applications.46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. July 25–28 2010 Nashville USA 2010–7121.
2. Design and optimization of variable thrust hybrid rocket motors for sounding rockets
3. Summarization on variable liquid thrust rocket engines
4. R. W. Carlson Method and System for Controlling Solid Propellant Thrust U. S. Patent 8584443 Digital Solid State Propulsion Reno 2013.
5. X. G. Wei G. Q. He J. Li Z. F. Zhou The Analysis on the Rising Section of Experimental Pressure in Variable Thrust Pintle Solid Rocket Motor.44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. July 21–23 2008 Hartford USA 2008–4604.
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