Study on the multi-start system of turbopump-fed rocket engine with storable propellants(PDF)
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
Issue:
2010年03期
Page:
15-18
Research Field:
Publishing date:
Info
Title:
Study on the multi-start system of turbopump-fed rocket engine with storable propellants
Author(s):
-
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V434
DOI:
-
Abstract:
For high level thrust requirement and long duration mission, the turbopump-fed rocket engine has more advantages than that of the pressure-fed rocket engine. To meet the need of the development of propulsion system for upper stage and heavy space vehicle, the engine should have the capability of multi-start. This paper aimed at the need for the multi-start capability of the storable propellant turbopump-fed rocket engine. Several different designs of the multi-start system were analyzed and efforts on the start-tank system development were described.