|Table of Contents|

Applications of self-pressurization in divert and attitude control system(PDF)

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

Issue:
2010年02期
Page:
15-1
Research Field:
研究与设计
Publishing date:

Info

Title:
Applications of self-pressurization in divert and attitude control system
Author(s):
Zou Yu;  Li Ping
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V434
DOI:
-
Abstract:
New self-pressurizing Divert and Attitude Control System (DACS)combines the performance advantage and lightweight of a turbopump rocket engine and the restartability advantage of a pressurized propellant system. New self-pressurizing divert and attitude control system reduces the size and mass of hardware by permitting the use of compact high pressure thrust chambers and reducing liquid tank pressures and minimizing inert gas storage. In this paper, the application advantages, technical characters, operation principle，current status of new lightweight divert and attitude control system are presented. And the key techniques are analyzed. Based on current technology status, the necessity, strategy and approach of future development are brought forward.

References:

[1]Whitehead J C. Performance of a New Lightweight Recip-rocating Pump[R]. AIAA2005-3921. [2]Whitehead J C. Reciprocating Pump Systems for Space Propulsion[R]. AIAA2004-3836. [3]Maj Michael C Lydon. Hydrogen Peroxide Self Pressuriz-ing Storage Tank[R]. AIAA2004-4201. [4]Whitehead J C, Colella N J, Pittenger L C. Design and Flight Testing of a Reciprocating Pump Fed Rocket[R]. AIAA94-3031. [5]Whitehead J C. Test Results for a Reciprocating Pump Powered by Decomposed Hydrogen Peroxide[R]. AIAA2001-3839. [6]Frei T E, Maybee J C, Whitehead J C. Recent Test Results of a Warm Gas Pumped Monopropellant Propulsion System[R]. AIAA94-3393. [7]Whitehead J C. Hydrogen Peroxide Gas Generator Cycle with a Reciprocating Pump[R]. AIAA2002-3702.

Memo

Memo:
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Last Update: 1900-01-01