Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm

Author:

Lee Jungpyo1,Rhee Sunjae2,Kim Jinkon3,Moon Heejang3

Affiliation:

1. University of Brasilia, Brasilia, Federal District, 70910-900, Brazil

2. Hanwha Corporation, Daejeon, 34060, Republic of Korea

3. Korea Aerospace University, Goyang-si, 10540, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Reference21 articles.

1. HumbleR.HenryG.LarsonW., Space Propulsion Analysis and Design, McGraw-Hill, Inc., New York, 1995, pp. 610–620, Chap. 7.

2. Fundamentals of Hybrid Boundary-Layer Combustion

3. Effect of Diaphragms on Regression Rate in Hybrid Rocket Motors

4. Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets

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