Experimental Characterization of Combustion Instabilities in High-Mass-Flux Hybrid Rocket Engines-Reference-Cited by-同舟云学术

Experimental Characterization of Combustion Instabilities in High-Mass-Flux Hybrid Rocket Engines

Published:2016-07 Issue:4 Volume:32 Page:958-966
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Fraters Arjan¹,Cervone Angelo¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35485

Reference19 articles.

1. Hybrid Rocket Fuel Regression Rate Data and Modeling

2. BettnerM.HumbleR. W. “Polyethylene and Hydrogen Peroxide Hybrid Testing at the United States Air Force Academy,” U.S. Air Force Academy Rept. 19990827-041, Colorado Springs, CO, 1998.

3. Design of a small H2O2/HTPB hybrid sounding rocket motor

4. Design and optimization of variable thrust hybrid rocket motors for sounding rockets

5. Peregrine Hybrid Rocket Motor Ground Test Results

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