Dynamic characteristics study of regression rate in variable thrust hybrid rocket motor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference29 articles.
1. Transient investigation of nozzle erosion in a long-time working hybrid rocket motor;Tian;Aero. Sci. Technol.,2021
2. Restitution methodology for space and time dependent solid-fuel port diameter evolution in hybrid rocket engines;Durand;Aero. Sci. Technol.,2021
3. Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number;Cai;Aero. Sci. Technol.,2020
4. Numerical and experimental investigation of throttleable hybrid rocket motor with aerospike nozzle;Tian;Aero. Sci. Technol.,2020
5. Design optimization of velocity-controlled cruise vehicle propelled by throttleable hybrid rocket motor;Xiao;Aero. Sci. Technol.,2021
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