Experimental research on the spray characteristics of pintle injector-Reference-Cited by-同舟云学术

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Experimental research on the spray characteristics of pintle injector

Published:2019-09 Issue: Volume:162 Page:424-435
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Chen Huiyuan,Li Qinglian,Cheng Peng

Funder

Chinese Program for New Century Excellent Talents in University

National Natural Science Foundation of China

National Basic Research Program of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Pintle injectors;Heister,2011

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

3. The lunar module descent engine – a historical perspective;Gilroy,1989

4. The descent engine for the lunar module;Elverum,1967

5. Characterization of pintle engine performance for nontoxic hypergolic bipropellants;Austin,2002

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

3. Spray characteristics of a multi-slit type throttleable pintle injector with different slit heights;Acta Astronautica;2024-02

4. Pintle Injector Performance Sensitivity to the Radial Injection Arrangement;AIAA SCITECH 2024 Forum;2024-01-04

5. NUMERICAL SIMULATIONS OF LIQUID FILM PRIMARY BREAKUP IN A PINTLE INJECTOR: A PARAMETRIC STUDY;Atomization and Sprays;2024

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