Latest progress of liquid apogee engine for satellites in SISP

Changguo Liu; Ting Zhao; Ruida Chen; Daren Yu

Latest progress of liquid apogee engine for satellites in SISP

Changguo Liu
, Ting Zhao
, Ruida Chen
, Daren Yu

School of Energy Science and Engineering

Shanghai Institute of Space Propulsion
Shanghai Engineering Research Center of Space Robotics
Harbin Institute of Technology

Research output: Contribution to journal › Conference article › peer-review

Abstract

Currently, liquid rocket engines with 490N thrust or the same level are widely used to provide thrust for spacecraft apogee injecting or other orbit maneuvers. Apogee engines used on the Chinese 3-axis stabilized geostationary satellites were supplied by Shanghai Institute of Space Propulsion(SISP). Until now two generation engines have been developed and the third generation engine is in development. The vacuum specific impulse of the three generation engines using propellant of MON-1/MMH is 305s, 315s and 323s respectively. Focusing on the development of 750N high-performance Liquid Apogee Engine(LAE) with niobium alloy, the specific impulse can reach more than 321s, and the working life can meet the requirements of 25000 seconds.

Original language	English
Journal	Proceedings of the International Astronautical Congress, IAC
Volume	2018-October
State	Published - 2018
Event	69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 - Bremen, Germany Duration: 1 Oct 2018 → 5 Oct 2018

Keywords

Flight
High Performance
Liquid Apogee Engine

Cite this

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title = "Latest progress of liquid apogee engine for satellites in SISP",

abstract = "Currently, liquid rocket engines with 490N thrust or the same level are widely used to provide thrust for spacecraft apogee injecting or other orbit maneuvers. Apogee engines used on the Chinese 3-axis stabilized geostationary satellites were supplied by Shanghai Institute of Space Propulsion(SISP). Until now two generation engines have been developed and the third generation engine is in development. The vacuum specific impulse of the three generation engines using propellant of MON-1/MMH is 305s, 315s and 323s respectively. Focusing on the development of 750N high-performance Liquid Apogee Engine(LAE) with niobium alloy, the specific impulse can reach more than 321s, and the working life can meet the requirements of 25000 seconds.",

keywords = "Flight, High Performance, Liquid Apogee Engine",

author = "Changguo Liu and Ting Zhao and Ruida Chen and Daren Yu",

note = "Publisher Copyright: Copyright {\textcopyright} 2018 by the International Astronautical Federation (IAF). All rights reserved.; 69th International Astronautical Congress: \#InvolvingEveryone, IAC 2018 ; Conference date: 01-10-2018 Through 05-10-2018",

year = "2018",

language = "英语",

volume = "2018-October",

journal = "Proceedings of the International Astronautical Congress, IAC",

issn = "0074-1795",

publisher = "International Astronautical Federation, IAF",

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TY - JOUR

T1 - Latest progress of liquid apogee engine for satellites in SISP

AU - Liu, Changguo

AU - Zhao, Ting

AU - Chen, Ruida

AU - Yu, Daren

PY - 2018

Y1 - 2018

N2 - Currently, liquid rocket engines with 490N thrust or the same level are widely used to provide thrust for spacecraft apogee injecting or other orbit maneuvers. Apogee engines used on the Chinese 3-axis stabilized geostationary satellites were supplied by Shanghai Institute of Space Propulsion(SISP). Until now two generation engines have been developed and the third generation engine is in development. The vacuum specific impulse of the three generation engines using propellant of MON-1/MMH is 305s, 315s and 323s respectively. Focusing on the development of 750N high-performance Liquid Apogee Engine(LAE) with niobium alloy, the specific impulse can reach more than 321s, and the working life can meet the requirements of 25000 seconds.

AB - Currently, liquid rocket engines with 490N thrust or the same level are widely used to provide thrust for spacecraft apogee injecting or other orbit maneuvers. Apogee engines used on the Chinese 3-axis stabilized geostationary satellites were supplied by Shanghai Institute of Space Propulsion(SISP). Until now two generation engines have been developed and the third generation engine is in development. The vacuum specific impulse of the three generation engines using propellant of MON-1/MMH is 305s, 315s and 323s respectively. Focusing on the development of 750N high-performance Liquid Apogee Engine(LAE) with niobium alloy, the specific impulse can reach more than 321s, and the working life can meet the requirements of 25000 seconds.

KW - Flight

KW - High Performance

KW - Liquid Apogee Engine

UR - https://www.scopus.com/pages/publications/85065319127

M3 - 会议文章

AN - SCOPUS:85065319127

SN - 0074-1795

VL - 2018-October

JO - Proceedings of the International Astronautical Congress, IAC

JF - Proceedings of the International Astronautical Congress, IAC

T2 - 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018

Y2 - 1 October 2018 through 5 October 2018

ER -

Latest progress of liquid apogee engine for satellites in SISP

Abstract

Keywords

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