|Table of Contents|

Experimental investigation and on-orbit flying validation of an ADN-based liquid space engine(PDF)

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

Issue:
2018年01期
Page:
8-14
Research Field:
专论与综述
Publishing date:

Info

Title:
Experimental investigation and on-orbit flying validation of an ADN-based liquid space engine
Author(s):
YAO Zhaopu;  ZHANG Wei;  WANG Meng;  CHEN Jun;  SHEN Yan
Beijing Institute of Control Engineering, Beijing 100190, China
Keywords:
ammonium dinitramide(ADN);  liquid space thruster;  experimental investigation;  on-orbit flying validation
PACS:
V511-34
DOI:
-
Abstract:
The experimental investigation and on-orbit flying validation of the ADN-based liquid space engine developed by Beijing Institute of Control Engineering(BICE)are introduced in this paper.The experiment research about the combustion mechanism of the combustion chamber of a 1N model thruster was performed with the measuring method of tunable diode laser absorption spectroscopy(TDLAS).The variation of characteristic parameters such as fuel gas temperature and component concentrations of CO and N2O in the combustion chamber with injection pressure were measured.The effects of the propellant inlet pressure on the combustion process were evaluated.The hot fire test results and main performance indexes of an ADN-based liquid thruster family including 0.2 N, 1 N, 5 N, and 20 N thrusters are presented.The performance data at different operation conditions were obtained.The on-orbit flying validation result of the 1N ADN-based liquid thruster is introduced for the first time.The contents in this paper are beneficial to the development of green aerospace propulsion techniques.

References:

[1] Yang R, Thakre P, Yang V. Thermal decomposition and combustion of ammonium dinitramide(Review)[J]. Combust explo shock, 2005, 41: 657-679.
[2] PARK J, CHAKRABORTY D, LIN M C. Thermal decomposition of gaseous ammonium dinitramide at low pressure [C]// Proceedings of Twenty-Seventh Symposium(International)on Combustion. [S.l.]: Combustion Institute, 1998: 2351-2357.
[3] SINDITSKII V P, EGORSHEV V Y, LEVSHENKOV A I, et al. Combustion of ammonium dinitramide, part 1: burning behavior [J]. Journal of propulsion power, 2006, 22: 769-776.
[4] SINDITSKII V P, EGORSHEV VY, LEVSHENKOV A I, et al. Combustion of ammonium dinitramide, part 2: combustion mechanism [J]. Journal of propulsion power, 2006, 22: 777-785.
[5] KOROBEINICHEV O P, BOLSHOVA TA, PALETSKY A A. Modeling the chemical reactions of ammonium dinitramide(ADN)in a flame [J]. Combust flame, 2001, 126: 1516-1523.
[6] THAKRE P, DUAN Y, YANG V. Modeling of ammonium dinitramide(ADN)monopropellant combustion with coupled condensed and gas phase kinetics [J]. Combust flame, 2014, 161: 347-362.
[7] WINGBORG N, JOHANSSON M, BODIN L. Initial development of a laboratory rocket thruster for ADN-based liquid monopropellant: FOI-R-2123-SE [R]. Sweden: Swedish Defence Research Agency, 2006.
[8] LARSSON A, WINGBORG N. Green propellants based on ammonium dinitramide(ADN)[M/OL]. [2011-02-14]. http://xueshu.baidu.com.
[9] YAO Z P, ZHANG W, WANG M, et al. Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion [J]. Aerosp Sci Technol, 2015, 45: 140-149.
[10] ZENG H, LI F, ZHANG S H, et al. Midinfrared absorption measurements of nitrous oxide in ammonium dinitramide monopropellant thruster [J]. Journal of propulsion power, 2015, 31: 1496-1500.
[11] JING L, HUO Y, WANG J L, et al. Experimental investigations on the evaporation and combustion processes of ammonium-dinitramide-based liquid propellant [J]. Journal of propulsion power, 2017, 33: 343-349.
[12] ANFLO K, PERSSON M, THORMAHLEN P, et al. Flight demonstration of an ADN-based Propulsion System: IAC-06-C4.108 [R]. [S.l.]: IAC, 2006.
[13] 徐峰,罗军,彭飞,火箭发动机试验红外测温技术应用[J],火箭推进,2017,43(1):,78-84.
XU, Feng, LUO, Jun, PENG, Fei. Application of Infrared Temperature Measurement Technology in Liquid Rocket Engine Test[J], Journal of rocket propulsion, 2017,43(1):,78-84.
[14] ZHOU X. Diode-laser absorption sensor for combustion control[D].USA: Standford University, 2005..

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