Liquid Sheet–Sheet Impinging Structure for Pintle Injector with Nontoxic Hypergolic Bipropellant
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea
2. Korea Institute of Machinery and Materials, Daejeon 34103, 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
Reference18 articles.
1. Pintle Injectors
2. TRW pintle engine heritage and performance characteristics
3. Characterization of Pintle Engine Performance for Nontoxic Hypergolic Bipropellants
4. Theoretical Investigation of Some High-Performance Novel Amine Azide Propellants
5. FlorczukW.RarataG. “Performance Evaluation of the Hypergolic Green Propellants Based on the HTP for a Future Next Generation Spacecrafts,” AIAA Paper 2017-4849, July 2017. 10.2514/6.2017-4849
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