Hybrid Gas Generator for a Staged Hybrid Rocket Engine-Reference-Cited by-同舟云学术

Hybrid Gas Generator for a Staged Hybrid Rocket Engine

Published:2017-01 Issue:1 Volume:33 Page:204-212
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Lee Dongeun¹,Lee Changjin¹

Affiliation:

1. Konkuk University, Seoul 143-701, Republic of Korea

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.B36036

Reference11 articles.

1. ShackelfordB. “The Hybrid Propulsion Technology Program, Phase 1,” Vol. 3, Rept. NAS8-37777, Ogden, UT, Nov. 1989.

2. “Hybrid Propulsion Technology Program,” Atlantic Research Corp. Rept. NAS8 37776, Gainesville, VA, Jan. 1990.

3. ShackelfordB. “The Hybrid Propulsion Technology Program, Phase 1,” Vol. 4, Rockwell International Corp. Rept. NAS8-37777, Canoga Park, CA, Nov. 1989.

4. Regression-Rate and Heat-Transfer Correlations for Hybrid Rocket Combustion

5. KuoK. K.LuY.ChiaveriniM. J.JohnsonD. K.SerinN.RishaG. A.MerkleC. L.VenkateswaranS. “Fundamental Phenomena on Fuel Decomposition and Boundary Layer Combustion Processes with Applications to Hybrid Rocket Motors,” The Pennsylvania State Univ., NAS8-39945, University Park, PA, June 1996.

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