Investigation on gas dynamic resonance tube ignition method

Guo Zhu Liang; Bin Ma; Guo Zhou Zhang; Xian Chen Cheng; Zhen Peng Zhang

Investigation on gas dynamic resonance tube ignition method

Guo Zhu Liang^*
, Bin Ma
, Guo Zhou Zhang
, Xian Chen Cheng
, Zhen Peng Zhang

^*Corresponding author for this work

School of Astronautics

Beihang University

Research output: Contribution to journal › Article › peer-review

7 Scopus citations

Abstract

To develop the new technology of gas dynamic resonance tube non-electric ignition for liquid rocket engines, a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co-axial gaseous oxygen-hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed.

Original language	English
Pages (from-to)	286-289
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	22
Issue number	4
State	Published - Aug 2001

Keywords

Aerodynamic heating
Ignition
Ignition system
Liquid propellant rocket engine

Cite this

@article{abf96741e5da4c7e827a899287189bfb,

title = "Investigation on gas dynamic resonance tube ignition method",

abstract = "To develop the new technology of gas dynamic resonance tube non-electric ignition for liquid rocket engines, a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co-axial gaseous oxygen-hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed.",

keywords = "Aerodynamic heating, Ignition, Ignition system, Liquid propellant rocket engine",

author = "Liang, \{Guo Zhu\} and Bin Ma and Zhang, \{Guo Zhou\} and Cheng, \{Xian Chen\} and Zhang, \{Zhen Peng\}",

year = "2001",

month = aug,

language = "英语",

volume = "22",

pages = "286--289",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "4",

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TY - JOUR

T1 - Investigation on gas dynamic resonance tube ignition method

AU - Liang, Guo Zhu

AU - Ma, Bin

AU - Zhang, Guo Zhou

AU - Cheng, Xian Chen

AU - Zhang, Zhen Peng

PY - 2001/8

Y1 - 2001/8

N2 - To develop the new technology of gas dynamic resonance tube non-electric ignition for liquid rocket engines, a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co-axial gaseous oxygen-hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed.

AB - To develop the new technology of gas dynamic resonance tube non-electric ignition for liquid rocket engines, a new conceptual scheme of combined nozzle mixing gas resonance heating was proposed. The gaseous helium resonance surface heating igniter and the co-axial gaseous oxygen-hydrogen resonance torch igniter were described. And the general engineering design criteria for the resonance tube igniter were proposed.

KW - Aerodynamic heating

KW - Ignition

KW - Ignition system

KW - Liquid propellant rocket engine

UR - https://www.scopus.com/pages/publications/0035436121

M3 - 文章

AN - SCOPUS:0035436121

SN - 1001-4055

VL - 22

SP - 286

EP - 289

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Investigation on gas dynamic resonance tube ignition method

Abstract

Keywords

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