Experimental study on the combustion and pressure drop characteristics of a pintle injector for LOX/kerosene rocket engine-Reference-Cited by-同舟云学术

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Experimental study on the combustion and pressure drop characteristics of a pintle injector for LOX/kerosene rocket engine

Published:2024-06 Issue: Volume:219 Page:208-219
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zhao Yaming,Yu Nanjia^ORCID,Li Tianwen,Zhou Chuang

Publisher

Elsevier BV

Reference38 articles.

1. A review of throttling technology development for large-thrust liquid rocket engines;Bin;Aero. China,2021

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

3. TRW pintle engine heritage and performance characteristics | Joint Propulsion Conferences;Dressier;AIAA Pap,2000

4. Summary of deep throttling rocket engines with emphasis on Apollo LMDE;Dressler,2006

5. The development of 7500 N variable thrust engine for Chang’E-3;Lei;Sci. Sin. Technol.,2014

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