Numerical investigation on regression rate and thrust regulation behaviors of a combined solid rocket motor with aluminum-based fuel

Author:

Zou Xiangrui,Wang Ningfei,Han Lei,Bai Taotao,Xie Kan

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Solid propellant chemistry, combustion, and motor interior ballistics;Brill,2000

2. An application of commercial grade hydrogen peroxide for hybrid/liquid rocket engine;Tsujikado,2002

3. Conceptual aerodynamic design of pintle nozzle for variable-thrust propulsion;Saravanan;Int. J. Aeronaut. Space Sci.,2020

4. An ascent guidance algorithm for the energy management of solid rockets;Cheng;ISA Trans.,2020

5. Scale effect of fuel regression rate in hybrid rocket motor;Cai;Aerosp. Sci. Technol.,2013

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