High Pressure Spray and Combustion Characteristics of Throttleable Pintle Injector-Reference-Cited by-同舟云学术

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High Pressure Spray and Combustion Characteristics of Throttleable Pintle Injector

Published:2022-04-30 Issue:2 Volume:26 Page:60-71
ISSN:1226-6027
Container-title:Journal of the Korean Society of Propulsion Engineers
language:en
Short-container-title:KSPE

Author:

Kim Dae Hwan,Heo Subeom,Kim Inho,Hwang Donghyun,Kang Cheolwoong,Lee Shinwoo,Ahn Kyubok,Yoon Youngbin

Funder

SNU Future Innovation Institute

Ministry of Science and ICT

Korea Aerospace Research Institute

Publisher

The Korean Society of Propulsion Engineers

Subject

General Medicine

Reference21 articles.

1. The Low Earth Orbit Satellite Population and Impacts of the SpaceX Starlink Constellation

2. Korean Reusable Launch Vehicle Development Strategy Using SpaceX’s Strategy

3. TRW pintle engine heritage and performance characteristics

4. Characterization of Pintle Engine Performance for Nontoxic Hypergolic Bipropellants

5. Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Development of a Numerical Method for Regenerative Cooling Channels with Phase Change of Throttleable Liquid Rocket Engine;Journal of the Korean Society of Propulsion Engineers;2023-12-31

2. Preliminary Test for System Design of Lab-Scale Vertical Landing Vehicle;Journal of the Korean Society of Propulsion Engineers;2023-12-31

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