ADN基发动机燃烧室CO组分实验测量
Concentration Measurement of Carbon Monoxide in Combustion Chamber of an ADN-Based Propellant Thruster
查看参考文献16篇
|
文摘
|
为研究ADN基发动机燃烧室内的燃烧过程,搭建了一套基于可调谐半导体激光器吸收光谱(TDLAS)实验测量系统。实验采用直接吸收光谱法对ADN基发动机燃烧室内CO组分摩尔分数进行测量,获得了喷注压力分别为1.1MPa,0.9MPa,0.7MPa,0.5MPa时,发动机燃烧室内CO组分摩尔分数随时间的变化。实验结果表明当发动机喷注压力由1.1MPa下降到0.5MPa时,燃烧室内CO平均摩尔分数由2%上升到4.7%,这表明发动机喷注压力的变化影响燃烧室内ADN基推进剂化学反应进程,当喷注压力下降时燃烧室内CO摩尔分数升高,ADN基推进剂燃烧不充分。 |
|
其他语种文摘
|
A tunable diode laser absorption spectroscopy (TDLAS) system was set up to investigate the combustion process of ADN-based propellant thruster. In the experiment,the mole fraction of CO was measured by using direct absorption scheme. The temporal variation of mole fraction of CO was experimentally obtained with respect to various injection pressure such as 1.1MPa,0.9MPa,0.7MPa,and 0.5MPa. Experimental results indicate that when the injection pressure was reduced from 1.1MPa to 0.5MPa,the average mole fraction of CO increased from 2% to 4.7%.It is shown that the injection pressure could have a crucial influence on the chemical reaction procedure of ADN-based propellant and the mole fraction of CO will arise as injection pressure decreases. Therefore,energy release of ADN-based propellant is insufficient in the case of low injection pressure. |
|
来源
|
推进技术
,2015,36(5):650-655 【核心库】
|
|
DOI
|
10.13675/j.cnki.tjjs.2015.05.002
|
|
关键词
|
量子级联激光器
;
ADN基发动机
;
绿色推进剂
;
吸收光谱
;
喷注压力
|
|
地址
|
1.
中国空间技术研究院北京控制工程研究所, 高温气体动力学国家重点实验室, 北京, 100190
2.
中国空间技术研究院北京控制工程研究所, 北京, 100190
3.
中国科学院力学研究所, 高温气体动力学国家重点实验室, 北京, 100190
|
|
语种
|
中文 |
|
文献类型
|
研究性论文 |
|
ISSN
|
1001-4055 |
|
学科
|
航天(宇宙航行) |
|
基金
|
国家973计划
|
|
文献收藏号
|
CSCD:5429441
|
参考文献 共
16
共1页
|
|
1.
陈兴强. 可用于替代肼的2种绿色单组元液体推进剂HAN、ADN.
化学推进剂与高分子材料,2011,9(4):63-66
|
CSCD被引
8
次
|
|
|
|
|
2.
Anflo K.
In-Space Demonstration of an ADN-Based Propulsion System. AIAA 2011-5832
|
CSCD被引
1
次
|
|
|
|
|
3.
Anflo K.
Towards Green Propulsion for Spacecraft with ADN-Based Monopropellants. AIAA 2002-3847
|
CSCD被引
1
次
|
|
|
|
|
4.
Gronland T A.
ADN-Based Propulsion for Spacecraft-Key Requirements and Experimental Verification. AIAA 2004-4145
|
CSCD被引
1
次
|
|
|
|
|
5.
Anflo K.
Flight Demonstration of an ADN-Based Propulsion System on the PRISMA Satellite. AIAA 2006-5212
|
CSCD被引
1
次
|
|
|
|
|
6.
Pokrupa N.
Spacecraft System Level Design with Regards to Incorporation of a New Green Propulsion System. AIAA 2011-6129
|
CSCD被引
1
次
|
|
|
|
|
7.
Persson M.
A Family of Thrusters for ADN-Based Monopropellant LMP-103S. AIAA 2012-3815
|
CSCD被引
3
次
|
|
|
|
|
8.
Korobeinichev O P. Study of Combustion Characteristics of Ammonium Dinitramide/Polycaprolactone Propellants.
Journal of Propulsion and Power,2003,19(2):203-212
|
CSCD被引
4
次
|
|
|
|
|
9.
姚兆普. 基于二硝酰胺铵(ADN)的无毒推进剂热分解及燃烧反应路径研究.
空间控制技术与应用,2013,5:53-57
|
CSCD被引
3
次
|
|
|
|
|
10.
Philippe L C. Laser Diode Wavelength Modulation Spectroscopy for Simultaneous Measurement of Temperature, Pressure, and Velocity in Shock-Heated Oxygen Flows.
Applied Optics,1993,32(30):6090-6103
|
CSCD被引
50
次
|
|
|
|
|
11.
Arroyo M P. Absorption Measurements of Water-Vapor Concentration, Temperature, and Line-Shape Parameters Using a Tunable In GaAsP Diode-Laser.
Applied Optics,1993,32(30):6104-6116
|
CSCD被引
24
次
|
|
|
|
|
12.
李飞.
近红外吸收光谱诊断技术在超燃中的应用,2009
|
CSCD被引
1
次
|
|
|
|
|
13.
李飞. 超燃燃烧室气流参数诊断.
力学学报,2011,43(6):1061-1067
|
CSCD被引
10
次
|
|
|
|
|
14.
李飞. TDLAS测量甲烷/空气预混平面火焰温度和H_2O浓度.
实验流体力学,2009,23(2)
|
CSCD被引
1
次
|
|
|
|
|
15.
Lin X. CO Concentration and Temperature Measurements in a Shock Tube for Martian Mixtures by Coupling OES and TDLAS.
Applied Physics B-lasers and Optics,2013,110(3):401-409
|
CSCD被引
5
次
|
|
|
|
|
16.
Xin Zhou.
Diode-Laser Absorption Sensor Combustion Control,2005
|
CSCD被引
1
次
|
|
|
|
|
了解气象卫星更多信息，请访问