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1
Mechanical properties and ablation properties of C/SiC-ZrC composites for hypersonic vehicle
YANG Xiaohui, WANG Fuyuan, WANG Yi, Cao Pei, BAI Longteng, ZHAO Qiang

2017 03 [59－66][Abstract](2685)[PDF:1282KB ](1679)
1679
2
Research overview of commercial satellite platform with all-electric propulsion system
ZUO Kun1, 2, WANG Min1, LI Min2, TANG Hai-bin2

2015 02 [13－20][Abstract](1814)[PDF:1805KB ](1599)
1599
3
Development and application of Hall electric propulsion technology
KANG Xiaolu1, 2, HANG Guanrong1, 2，ZHU Zhichun1, 2

2017 01 [8－17][Abstract](1928)[PDF:2378KB ](1589)
1589
4
Research progress on ignition of HAN-based green propellant
WANG Xinqiang,DENG Kangqing,LI Hongxu,YU Xiaobo

2017 02 [72－76][Abstract](1937)[PDF:330KB ](1307)
1307
5
esearch on plume flow of space thrusters
GUO Jing, KONG Fan-chao, HU Xu-kun

2014 06 [46－50][Abstract](1200)[PDF:1373KB ](1283)
1283
6
On-board gauging method of remaining propellant
YUAN Lei, WANG Shen, LIAN Ren-zhi, LIU Tao

2013 05 [75－81][Abstract](894)[PDF:1273KB ](1264)
1264
7
Digital measurement system for cryogenic liquid level
DUAN Wenhao, ZHANG Jia, WANG Hongyue

2017 03 [79－82][Abstract](1427)[PDF:1004KB ](1176)
1176
8
Design method of waverider with controlled horizontal projection of leading edge
LI Yongzhou1,LI Guangxi1,ZHANG Kunyuan2,SUN Di3

2017 05 [20－27][Abstract](991)[PDF:2009KB ](1172)
1172
9
Overview of modeling and simulation technology for propellant pressurization feed system of liquid rocket engine
GUO Jing, SONG Jingjing, KONG Fanchao

2015 05 [1－6][Abstract](1748)[PDF:413KB ](1166)
1166
10
Application of AMESim in dynamic characteristic simulation of liquid rocket engine system
PAN Hui, ZHANG Li-hui

2011 03 [6－11][Abstract](1296)[PDF:454KB ](1158)
1158
11
Comparative study on electric pump and pressure-fed propulsion systems
LIU Changbo

2017 02 [32－39][Abstract](1170)[PDF:451KB ](1123)
1123
12
Development of 1 000 N bipropellant orbit control engine with light weight and high specific impulse
LIU Xiaowei, YAO Mingming, LI Jiaming, CAO Jing, QU Haijun

2015 04 [8－12][Abstract](880)[PDF:1621KB ](1096)
1096
13
Multiple-working-conditions flowrate control for liquid engine test
JI Jun-feng, WU Guang-zhong, MA Li-ya, LI Jiu-long, LIN Meng, YOU Liang-ping

2011 02 [71－75][Abstract](1035)[PDF:262KB ](1094)
1094
14
Research on wear mechanism of mechanical seal for turbopump in liquid rocket engine
ZHAO Weigang1, ZHANG Pengpeng2, REN Shanshan2, DONG Guangneng2

2017 03 [10－16][Abstract](1333)[PDF:1019KB ](1077)
1077
15
Failure analysis on stem of valve AA9-683
DONG Dong, LIU Hongwei, ZHANG Junfeng, LI Qian, ZHU Chengliang

2015 06 [99－104][Abstract](906)[PDF:1318KB ](1068)
1068
16
Preliminary design for composite thrust frame of liquid rocket engine
MU Penggang, LI Binchao, DU Dahua, DENG Changhua

2017 03 [35－41][Abstract](1325)[PDF:1206KB ](1064)
1064
17
Development, application, and prospect of expander cycle engine technology
ZHOU Limin,LIU Zhongxiang

2016 01 [1－5][Abstract](984)[PDF:265KB ](1058)
1058
18
Performance analysis of RBCC engine
Huang Wei,Luo Shibin,Wang Zhenguo

2007 05 [6－10][Abstract](997)[PDF:202KB ](1043)
1043
19
Application of RBCC and TBCC engines to RLVs
Chen Hong1，He Guoqiang2

2008 03 [39－43][Abstract](1248)[PDF:267KB ](1042)
1042
20
Application and development trend of space electric propulsion technology
TIAN Li-cheng, WANG Xiao-yong, ZHANG Tian-ping

2015 03 [7－14][Abstract](765)[PDF:527KB ](1034)
1034
21
Method to enhance combustion stability margin of high thrust rocket engine
LI Long-fei, CHEN Jian-hua, LIU Zhan-guo

2014 05 [8－13][Abstract](787)[PDF:765KB ](1015)
1015
22
Research and application of manufacturing technique for precision spherical parts
XU Hongxiang,ZHAO Baoke,ZHAO Fei,WU Ping,ZHANG Hang

2016 05 [88－91][Abstract](910)[PDF:2020KB ](1007)
1007
23
Design on streamline tracing inward turning inlet with controlled horizontal projection of intake
LI Yongzhou1,2, LI Guangxi1, ZHANG Kunyuan2, MA Yuan1

2017 03 [28－34][Abstract](865)[PDF:1145KB ](997)
997
24
Noise detection in test of liquid rocket engine
CHEN Hai-feng，LIU Xiao，ZHAO Zheng-she，ZHANG Shao-bo，XIN Xin

2014 03 [83－87][Abstract](886)[PDF:2650KB ](995)
995
25
Study on electron beam welding process for surface tension tank
YU Kang, XIE Ronghua, CHEN Xiaojiang

2015 05 [89－94][Abstract](1134)[PDF:1185KB ](992)
992
26
Application of infrared temperature measurement technology in liquid rocket engine test
XU Feng,LUO Jun,PENG Fei

2017 01 [78－84][Abstract](883)[PDF:396KB ](982)
982
27
Exploration of thrust drag characteristic of rocket ramjet combined cycle dynamic system
ZHANG Mengzheng,LU Yuanyuan,DU Quan,YANG Jianwen

2016 03 [1－5][Abstract](559)[PDF:1198KB ](980)
980
28
Automatic detecting system for wall thickness of pressure tube
YUAN Xiaoxiao1,2, LIU Qingyan3

2017 02 [52－58][Abstract](676)[PDF:1726KB ](951)
951
29
Frequency response characteristics of variable thrust engine with gas generator cycle
HUANG Xixuan, HUANG Minchao, Hu Xiaoping

2020 02 [29－35][Abstract](562)[PDF:1557KB ](945)
945
30
Static mechanical characteristics of turbopump seal assembly in liquid rocket engine
XU Yunfei1, 2, LIU Li1, XU Xuejun1, 2, LI Feng1, 2, HUANG Daoqiong1, 2, DUAN Jie3

2017 03 [17－21][Abstract](776)[PDF:734KB ](933)
933
31
Influence of temperature on tank pressurization system
MU Penggang, TONG Fei, PU Guangrong, MA Jian

2015 04 [74－78][Abstract](1167)[PDF:1989KB ](932)
932
32
Challenge and perspective of combined cycle propulsion system
Zhang Mengzheng，Li Ping，Chen Zukui

2009 01 [1－8][Abstract](975)[PDF:670KB ](928)
928
33
Progress of optimization for bipropellant uniform propulsion system
YUAN Lei, WANG Shen, LIU Tao, LIAN Ren-zhi

2014 06 [7－10][Abstract](1065)[PDF:1628KB ](926)
926
34
Conceptual schemes of China lunar excursion module descent engine
LIU Chang-bo,LAN Xiao-hui,LI Fu-yun

2011 02 [8－13][Abstract](1111)[PDF:371KB ](924)
924
35
Numerical simulation of air turbo rocket engine at windmilling state
ZHANG Liuhuan, LU Wanruo

2015 06 [16－20][Abstract](1064)[PDF:1644KB ](913)
913
36
Research on formation mechanism of negative pressure phenomenon in propellant pipeline
CAO Wei, WANG Rui, CHEN Jian, WEI Yanxiang, JIN Guangming, LIU Feng

2015 04 [37－42][Abstract](991)[PDF:1630KB ](907)
907
37
Parametrization sculpting software development for inducer based on Pro/E
ZHUANG Su-guo, LUO Peng, HOU Ning-tao, Yang Xia-hui

2014 03 [68－72][Abstract](968)[PDF:1574KB ](906)
906
38
Fault diagnosis of local resonance based on rotordynamic analysis
JIN Lu，ZHU Donghua，WANG Wei，HUANG Jinping，XUAN Tong

2017 03 [6－9][Abstract](724)[PDF:622KB ](899)
899
39
Integration design system for turbo pump in rocket engine
ZHANG Chenxi1, MA Xiaodan2

2015 04 [79－83][Abstract](1437)[PDF:1572KB ](896)
896
40
Analysis of effects of bellows in front of pump on thrust measurement
SHEN Jibin, ZENG Xiaojun, CAO Qinghong

2015 04 [95－99][Abstract](910)[PDF:1125KB ](895)
895
41
Research of bursting pressure stability for membrane valve
BAI Shaoqing, SUN Liang

2015 06 [46－50][Abstract](795)[PDF:1206KB ](893)
893
42
Combustion phenomena of kerosene and UDMH droplets in supercritical environment
ZHANG Meng-zheng1, XU Sheng-li2

2013 05 [1－6][Abstract](654)[PDF:1814KB ](892)
892
43
Development Status and Trends of Liquid Propellant

2004年01期 [1－6][Abstract](1844)[PDF:419KB ](885)
885
44
Development of non-friction S-spring valve
HUANG Aiqing, CAO Ming, TANG Meifang, YOU Gang

2015 06 [41－45][Abstract](919)[PDF:1138KB ](882)
882
45
Study on sealing design of cryogenic safety valve
YU Jingping ZHAO Yichun DAI Limin

2015 06 [55－60][Abstract](869)[PDF:1754KB ](880)
880
46
Reliability validation and assessment of pyrovalve used in missile, rocket and satellite
HUANG Qingwei, YUAN Hongbin, LI Hai

2015 06 [51－54][Abstract](966)[PDF:1219KB ](876)
876
47
Method of man-machine-environment control over foreign object debris in pipelines used in rocket engine test
QIN Yongtao, SONG Yang, SU Hongfang, LI Rong

2015 06 [80－85][Abstract](1142)[PDF:396KB ](865)
865
48
Research on control measures for equal expulsion of propellant in paralleled metal diaphragm tank
ZHANG Rongrong, REN Feng, ZHANG Liang

2015 06 [35－40][Abstract](1003)[PDF:1272KB ](858)
858
49
Performance analysis of ATR engine working with cracking gas of hydrocarbon fuel
ZHANG Liuhuan1, LIU Yan2, ZHANG Mengzheng1

2017 03 [1－5][Abstract](873)[PDF:799KB ](852)
852
50
Calculation of fuel gas thermodynamic parameters and transport coefficients for oxygen/kerosene engine
WANG Xin, ZOU Yanghui

2017 04 [34－40][Abstract](1141)[PDF:704KB ](848)
848