Numerical investigations of hybrid rocket engines
Author:
Funder
Russian Foundation for Basic Research
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference17 articles.
1. Integrated approach for hybrid rocket technology development;Barato;Acta Astronaut.,2016
2. Transient analysis on ignition process of catalytic hybrid rocket motor;Cai;Aero. Sci. Technol.,2017
3. Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor;Tian;Acta Astronaut.,2017
4. Extinction–reignition superiority in a single-stage sounding hybrid rocket;Chiba;Aero. Sci. Technol.,2016
5. Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor;Sun;Acta Astronaut.,2016
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