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Hydraulic test research on dynamic characteristics of oxygen pump of liquid rocket engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2013年03期
Page:
50-57
Research Field:
研究与设计
Publishing date:

Info

Title:
Hydraulic test research on dynamic characteristics of oxygen pump of liquid rocket engine
Author(s):
DU Da-hua HUANG Jin-ping XING Li-xiang XU Hao-hai
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
-
PACS:
V434-34
DOI:
-
Abstract:
In order to obtain the essential dynamic transfer function of the engine pump which is necessary for POGO stability analysis of the new generation large launch vehicle and dynamics research of the liquid rocket engine, a hydraulic test for the dynamic characteristics of a full-scale LOX/kerosene staged combustion cycle engine pump with speed drop-down was conducted, in which normal temperature water is taken as the test medium. The hydraulic test theory, simulation criterion, isolation tank design, exciting system design, control and measurement analysis system design, test details and data analysis method are thoroughly discussed in this paper. The POGO dynamic characteristics parameters and their disciplinarian laws of the oxygen pump were successfully identified through the test, which would be helpful to other hydraulic test and the real medium test.

References:

[1]OTSUKA S, TSUJIMOTO Y, KAMIJO K, et al. Frequency dependence of mass flow gain factor and cavitation compliance of cavitating inducers[J]. Journal of Fluids Engineering, 1996 (6): 400-408.
[2]DOTSON K W, RUBIN S, SAKO B H. Effects of unsteady pump cavitation on propulsion-structure interaction (POGO) in liquid rockets, AIAA2004-2027[R]. USA: AIAA, 2004.
[3]RUBIN Sheldon. An interpretation of transfer function data for a cavitating pump, AIAA2004-4025[R]. USA: AIAA, 2004.
[4]SHIMURA Takashi. Geometry effects in the dynamic response of cavitating LE-7 liquid oxygen pump[J]. Journal of Propulsion and Power, 1995 (2): 330-336.
[5]IACOPOZZI M, LIGNAROLO V, PREVEL D. POGO characterization of ARIANE Ⅴ turbopump LOX pump with hot water, AIAA 93-2124[R]. USA: AIAA, 1993.

Memo

Memo:
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Last Update: 1900-01-01