Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines
Author:
Affiliation:
1. Korea Aerospace University, Goyang, Gyeonggi-do 10540, Republic of Korea
2. Sungkyunkwan University, Suwon, Gyeonggi-do 16419, Republic of Korea
3. Andong National University, Andong, Gyeongsangbuk-do 36729, Republic of Korea
Funder
National Research Foundation of Korea
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.B36301
Reference28 articles.
1. Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review
2. The Lunar Module descent engine - A historical summary
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4. TRW pintle engine heritage and performance characteristics
5. Testing of the 650 Klbf LOX/LH2 low cost pintle engine
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