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1
Development and application of Hall electric propulsion technology
KANG Xiaolu1, 2, HANG Guanrong1, 2，ZHU Zhichun1, 2

2017 01 [8－17][Abstract](2647)[PDF:2378KB ](2203)
2203
2
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](3157)[PDF:1282KB ](1979)
1979
3
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](2242)[PDF:1805KB ](1869)
1869
4
Research progress on ignition of HAN-based green propellant
WANG Xinqiang,DENG Kangqing,LI Hongxu,YU Xiaobo

2017 02 [72－76][Abstract](2313)[PDF:330KB ](1598)
1598
5
esearch on plume flow of space thrusters
GUO Jing, KONG Fan-chao, HU Xu-kun

2014 06 [46－50][Abstract](1686)[PDF:1373KB ](1544)
1544
6
On-board gauging method of remaining propellant
YUAN Lei, WANG Shen, LIAN Ren-zhi, LIU Tao

2013 05 [75－81][Abstract](1037)[PDF:1273KB ](1456)
1456
7
Application of AMESim in dynamic characteristic simulation of liquid rocket engine system
PAN Hui, ZHANG Li-hui

2011 03 [6－11][Abstract](1606)[PDF:454KB ](1451)
1451
8
Digital measurement system for cryogenic liquid level
DUAN Wenhao, ZHANG Jia, WANG Hongyue

2017 03 [79－82][Abstract](1742)[PDF:1004KB ](1441)
1441
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](2115)[PDF:413KB ](1430)
1430
10
Performance analysis of RBCC engine
Huang Wei,Luo Shibin,Wang Zhenguo

2007 05 [6－10][Abstract](1149)[PDF:202KB ](1381)
1381
11
Design method of waverider with controlled horizontal projection of leading edge
LI Yongzhou1,LI Guangxi1,ZHANG Kunyuan2,SUN Di3

2017 05 [20－27][Abstract](1262)[PDF:2009KB ](1362)
1362
12
Comparative study on electric pump and pressure-fed propulsion systems
LIU Changbo

2017 02 [32－39][Abstract](1361)[PDF:451KB ](1351)
1351
13
Preliminary design for composite thrust frame of liquid rocket engine
MU Penggang, LI Binchao, DU Dahua, DENG Changhua

2017 03 [35－41][Abstract](1518)[PDF:1206KB ](1331)
1331
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](1553)[PDF:1019KB ](1331)
1331
15
Frequency response characteristics of variable thrust engine with gas generator cycle
HUANG Xixuan, HUANG Minchao, Hu Xiaoping

2020 02 [29－35][Abstract](763)[PDF:1557KB ](1305)
1305
16
Application of RBCC and TBCC engines to RLVs
Chen Hong1，He Guoqiang2

2008 03 [39－43][Abstract](1444)[PDF:267KB ](1302)
1302
17
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](1109)[PDF:1621KB ](1295)
1295
18
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](1179)[PDF:262KB ](1274)
1274
19
Development, application, and prospect of expander cycle engine technology
ZHOU Limin,LIU Zhongxiang

2016 01 [1－5][Abstract](1106)[PDF:265KB ](1266)
1266
20
Failure analysis on stem of valve AA9-683
DONG Dong, LIU Hongwei, ZHANG Junfeng, LI Qian, ZHU Chengliang

2015 06 [99－104][Abstract](1029)[PDF:1318KB ](1257)
1257
21
Study on electron beam welding process for surface tension tank
YU Kang, XIE Ronghua, CHEN Xiaojiang

2015 05 [89－94][Abstract](1335)[PDF:1185KB ](1231)
1231
22
Application and development trend of space electric propulsion technology
TIAN Li-cheng, WANG Xiao-yong, ZHANG Tian-ping

2015 03 [7－14][Abstract](1055)[PDF:527KB ](1222)
1222
23
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](987)[PDF:765KB ](1215)
1215
24
Automatic detecting system for wall thickness of pressure tube
YUAN Xiaoxiao1,2, LIU Qingyan3

2017 02 [52－58][Abstract](786)[PDF:1726KB ](1211)
1211
25
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](1056)[PDF:2020KB ](1186)
1186
26
Influence of temperature on tank pressurization system
MU Penggang, TONG Fei, PU Guangrong, MA Jian

2015 04 [74－78][Abstract](1397)[PDF:1989KB ](1179)
1179
27
Integration design system for turbo pump in rocket engine
ZHANG Chenxi1, MA Xiaodan2

2015 04 [79－83][Abstract](1807)[PDF:1572KB ](1171)
1171
28
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](973)[PDF:1145KB ](1169)
1169
29
Challenge and perspective of combined cycle propulsion system
Zhang Mengzheng，Li Ping，Chen Zukui

2009 01 [1－8][Abstract](1095)[PDF:670KB ](1168)
1168
30
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](1115)[PDF:2650KB ](1165)
1165
31
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](646)[PDF:1198KB ](1154)
1154
32
Application of infrared temperature measurement technology in liquid rocket engine test
XU Feng,LUO Jun,PENG Fei

2017 01 [78－84][Abstract](1132)[PDF:396KB ](1149)
1149
33
Progress of optimization for bipropellant uniform propulsion system
YUAN Lei, WANG Shen, LIU Tao, LIAN Ren-zhi

2014 06 [7－10][Abstract](1562)[PDF:1628KB ](1147)
1147
34
Conceptual schemes of China lunar excursion module descent engine
LIU Chang-bo,LAN Xiao-hui,LI Fu-yun

2011 02 [8－13][Abstract](1266)[PDF:371KB ](1137)
1137
35
Application of additive manufacturing technology in liquid rocket engine
ZUO Wei, SONG Menghua, YANG Huanqing, CHEN Xinhong

2018 02 [55－65][Abstract](1735)[PDF:32055KB ](1117)
1117
36
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](1042)[PDF:734KB ](1114)
1114
37
Development Status and Trends of Liquid Propellant

2004年01期 [1－6][Abstract](1987)[PDF:419KB ](1106)
1106
38
Study on pressurization of new generation launch vehicle
FAN Rui-xiang，TIAN Yu-rong，HUANG Bing

2012 04 [9－16][Abstract](1341)[PDF:486KB ](1105)
1105
39
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](1128)[PDF:1630KB ](1104)
1104
40
Calculation of fuel gas thermodynamic parameters and transport coefficients for oxygen/kerosene engine
WANG Xin, ZOU Yanghui

2017 04 [34－40][Abstract](1602)[PDF:704KB ](1103)
1103
41
Challenge to propulsion technology for vertical landing reusable launch vehicle
GAO Zhao-hui1, 2, LIU Yu1, XIAO Xiao2, WANG Xiao-wei2, SHEN Lin2

2015 03 [1－6][Abstract](1427)[PDF:351KB ](1097)
1097
42
Numerical simulation of air turbo rocket engine at windmilling state
ZHANG Liuhuan, LU Wanruo

2015 06 [16－20][Abstract](1193)[PDF:1644KB ](1092)
1092
43
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](1101)[PDF:1574KB ](1091)
1091
44
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](1375)[PDF:396KB ](1085)
1085
45
Research of bursting pressure stability for membrane valve
BAI Shaoqing, SUN Liang

2015 06 [46－50][Abstract](925)[PDF:1206KB ](1081)
1081
46
Fault diagnosis of local resonance based on rotordynamic analysis
JIN Lu，ZHU Donghua，WANG Wei，HUANG Jinping，XUAN Tong

2017 03 [6－9][Abstract](860)[PDF:622KB ](1081)
1081
47
Development of non-friction S-spring valve
HUANG Aiqing, CAO Ming, TANG Meifang, YOU Gang

2015 06 [41－45][Abstract](1126)[PDF:1138KB ](1074)
1074
48
Research progress of nitrous oxide propulsion technology
SONG Chang-qing, XU Wan-wu, ZHANG Jia-qi, CHEN Jian

2014 02 [7－15][Abstract](1601)[PDF:2348KB ](1072)
1072
49
Consideration on development of reusable liquid rocket engine in China
LI Bin1, ZHANG Xiaoping2, GAO Yushan2

2017 01 [1－7][Abstract](1208)[PDF:469KB ](1064)
1064
50
Analysis of effects of bellows in front of pump on thrust measurement
SHEN Jibin, ZENG Xiaojun, CAO Qinghong

2015 04 [95－99][Abstract](1076)[PDF:1125KB ](1060)
1060