|Table of Contents|

Computational simulation of a nontoxic propellant pump-fed variable-thrust engine(PDF)

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

Issue:
2009年06期
Page:
1-4
Research Field:
研究与设计
Publishing date:

Info

Title:
Computational simulation of a nontoxic propellant pump-fed variable-thrust engine
Author(s):
Tang Hu;  Zhang Tao;  Ren Yong
Xi′an Aerospace Propulsion Institute, Xi′an 710100, China
Keywords:
-
PACS:
V439
DOI:
-
Abstract:
The mathematical models of the main components are established based on a nontoxic propellant pump-fed variable-thrust engine system in this paper. Then the simulation is carried out according to the models and the main influence factors in the working process are investigated. The results indicate that the engine subassembly can work harmoniously, but the start-up process is slow. The jump time is long when the engine varies thrust. Larger valume of start-tank results in less start-up time.

References:

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Memo

Memo:
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Last Update: 1900-01-01