Optical Measurements of Ethanol/Liquid Oxygen Rocket Engine Combustor with Planar Pintle Injector-Reference-Cited by-同舟云学术

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Optical Measurements of Ethanol/Liquid Oxygen Rocket Engine Combustor with Planar Pintle Injector

Published:2015-07-23 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Sakaki Kazuki,Kakudo Hiromitsu,Nakaya Shinji,Tsue Mitsuhiro,Isochi Hikaru,Suzuki Kyohei,Makino Kazunori,Hiraiwa Tetsuo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3845

Reference23 articles.

1. Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review

2. On porous liquid propellant rocket engine injectors

3. Impinging Atomization Enhanced by Microjet Injection - effect, mechanism and optimization -

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1. Transient spray combustion characteristics in a gas–liquid pintle rocket engine under acoustic excitation;Scientific Reports;2024-06-07

2. Characterization of the Spray Flow Field at the Exit of a Pintle Injector;Lecture Notes in Mechanical Engineering;2024

3. Characterization of pintle engine performance for GO2/kerosene propellants;Applied Thermal Engineering;2023-06

4. Design of pintle injector using Kerosene-LOx as propellant and solving the problem of pintle tip thermal damage in hot firing test;Acta Astronautica;2022-12

5. Review of atomization and mixing characteristics of pintle injectors;Acta Astronautica;2022-11

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