Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor

Author:

Zhao Zeng,Cai Guobiao,Zhao Bo,Liu Yufei,Yu Nanjia

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Early developments in hybrid propulsion technology at the air force rocket propulsion laboratory;Mead,1995

2. Hybrid Rocket Development History;Altman,1991

3. Utilization of additive manufacturing in hybrid rocket technology: a review;Oztan;Acta Astronaut.,2021

4. 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

5. Effect of multi-location swirl injection on the performance of hybrid rocket motor;Vignesh;Acta Astronaut.,2020

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