Spray characteristics of a pintle injector based on annular orifice area-Reference-Cited by-同舟云学术

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Spray characteristics of a pintle injector based on annular orifice area

Published:2020-02 Issue: Volume:167 Page:201-211
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Lee Suji,Kim Daehwan,Koo Jaye,Yoon Youngbin

Funder

Advanced Research Center Program

National Research Foundation of Kore

Korea governmen

Advanced Space Propulsion Research Center

Seoul National University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Liquid-propellant rocket engine throttling: a comprehensive review;Casiano;J. Propuls. Power,2010

2. TRW pintle engine heritage and performance characteristics;Dressler,2000

3. Liquid Propellant Rocket Combustion Instability;Harrje,1972

4. SpaceX - Making Commercial Spaceflight a Reality;Seedhouse,2013

5. Northrop Grumman TR202 LOX/LH2 deep throttling engine technology project status;Gromski,2010

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1. Effects of slit geometric parameters on spray characteristics of double-slit pintle injectors;Experimental Thermal and Fluid Science;2025-01

2. Multi‒scale numerical investigations on the atomization performance of liquid‒liquid pintle injector;Aerospace Science and Technology;2024-11

3. Experimental study on the droplet size distribution of radial orifice gas–liquid pintle injector at ambient pressure;Experimental Thermal and Fluid Science;2024-06

4. Performance evaluation of modified pintle-type fuel injector for LRE (liquid rocket engine);Physics of Fluids;2024-05-01

5. Impact of chemical modeling on the numerical analysis of a LOx/GCH4 rocket engine pintle injector;Acta Astronautica;2024-05

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