|Table of Contents|

Development and in-orbit verification of orbit-control engine in YZ-3 upper stage(PDF)

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

Issue:
2020年03期
Page:
11-18
Research Field:
研究与设计
Publishing date:

Info

Title:
Development and in-orbit verification of orbit-control engine in YZ-3 upper stage
Author(s):
Hui1; 2; WU Erlong1; 2
(1. Shanghai Institute of Space Propulsion, Shanghai 201112, China; 2.Shanghai Engineering Research Center of Space Engine, Shanghai 201112, China)
Keywords:
YZ-3:upper stage;  orbit-control engine;  in-orbit verification
PACS:
V439.7
DOI:
-
Abstract:
The technical development of the upper stage and its orbit-control engine at home and abroad is reviewed in this paper. Based on the mission characteristics of YZ-3 upper stage, the technical scheme of 5 000 N upper stage engine is put forward, focusing on its ground tests and the first flight application. The development experience of YZ-3 upper stage engine is summarized for the reference of similar rocket engine development. Since the 5 000 N upper stage engine of YZ-3 adopts the extruded propellant supply system, orifice injector,regenerative cooling and C/SiC composite nozzle,it has the advantages of simple structure,multiple ignitions,large scale two-way swing. The first application flight was carried on December 29,2018

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Last Update: 2020-06-25