Dynamic Response of a Dual-Manifold Injector Rocket Engine to Throttling
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
2. China Aerodynamics Research & Development Center, 621000 Mianyang, People’s Republic of China
Funder
National Natural Science Foundation of China
National Basic Research Program of China
Program for New Century Excellent Talents in University
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36799
Reference31 articles.
1. Injectors and Combustion Performance of Rocket Thruster for Rocket-Ramjet Combined-Cycle Engine Model
2. Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine
3. Equivalence ratio and constriction effects on RBCC thrust augmentation
4. Experimental Investigation of an Alternative Rocket Configuration for Rocket-Based Combined Cycle Engines
5. Experiments with Ejector Rocket Entrainment
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