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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)
2685
2
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)
1937
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)
1928
4
Development Status and Trends of Liquid Propellant

2004年01期 [1－6][Abstract](1844)[PDF:419KB ](885)
1844
5
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)
1814
6
Thrust Calculation of Liquid Rocket Engine post Flight
Bu Nailan

2004年05期 [18－21][Abstract](1806)[PDF:36KB ](677)
1806
7
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)
1748
8
Integration design system for turbo pump in rocket engine
ZHANG Chenxi1, MA Xiaodan2

2015 04 [79－83][Abstract](1437)[PDF:1572KB ](896)
1437
9
Digital measurement system for cryogenic liquid level
DUAN Wenhao, ZHANG Jia, WANG Hongyue

2017 03 [79－82][Abstract](1427)[PDF:1004KB ](1176)
1427
10
Research progress of nitrous oxide propulsion technology
SONG Chang-qing, XU Wan-wu, ZHANG Jia-qi, CHEN Jian

2014 02 [7－15][Abstract](1358)[PDF:2348KB ](816)
1358
11
Application of additive manufacturing technology in liquid rocket engine
ZUO Wei, SONG Menghua, YANG Huanqing, CHEN Xinhong

2018 02 [55－65][Abstract](1344)[PDF:32055KB ](766)
1344
12
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)
1333
13
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)
1325
14
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)
1296
15
Clustering analysis for fault data in steady process of liquid propellant rocket engine
ZHANG Xiang, XU Hong-ping, AN Xue-yan, GENG Hui, ZHANG Su-ming

2015 02 [118－122][Abstract](1256)[PDF:276KB ](751)
1256
16
Research progress on numerical simulation technology of liquid rocket engine dynamic characteristics
LI Yuanqi,LIU Hongjun,XU Haohai,CHEN Hongyu

2017 05 [1－6][Abstract](1251)[PDF:1434KB ](690)
1251
17
Application of RBCC and TBCC engines to RLVs
Chen Hong1，He Guoqiang2

2008 03 [39－43][Abstract](1248)[PDF:267KB ](1042)
1248
18
Research on thermal protection behavior of silicide coating on Nb-W alloys used at high temperature
PAN Zhao-yi, CAI Gang, MA Shuang-min, SONG Guo-xin

2015 03 [59－65][Abstract](1240)[PDF:2214KB ](653)
1240
19
Application status and key technology of bipropellant blowdown propulsion systems
YANG Jun,HE Yongying,LIAN Renzhi,YANG Fushu

2016 04 [21－25][Abstract](1222)[PDF:3119KB ](760)
1222
20
Application of Nano-technology in Liquid Propellant Rocket Engine
Huang Zhiyong,Hu Zhongbing

2004年05期 [36－39][Abstract](1207)[PDF:40KB ](415)
1207
21
esearch on plume flow of space thrusters
GUO Jing, KONG Fan-chao, HU Xu-kun

2014 06 [46－50][Abstract](1200)[PDF:1373KB ](1283)
1200
22
Analysis on thermodynamic cycle characteristics of synergistic air-breathing rocket engine
GUO Hai-bo1, XIAO Hong2, NAN Xiang-yi1, LU Wan-ruo1

2013 03 [15－20][Abstract](1192)[PDF:809KB ](688)
1192
23
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](1174)[PDF:351KB ](752)
1174
24
Method of onboard propellant consumption calculation for Chang'e-3 propulsion system
CAO Wei1, XU Ying-qiao2, WEI Yan-xiang1, GUO Shang-qun1, JIN Guang-ming1

2015 01 [63－69][Abstract](1173)[PDF:911KB ](743)
1173
25
Research on a novel bipropellant for spacecrafts
HUANG Ji-qing, BAO Shi-guo, LIU Han-lin, LIU Jiang-qiang

2013 03 [67－71][Abstract](1172)[PDF:325KB ](660)
1172
26
Comparative study on electric pump and pressure-fed propulsion systems
LIU Changbo

2017 02 [32－39][Abstract](1170)[PDF:451KB ](1123)
1170
27
Establishment and confirmation of mathematical computational model of thickness of CVD-PyC interface and SiC coatings
YANG Xiao-hui, WANG Yi, BAI Long-teng

2014 05 [69－74][Abstract](1169)[PDF:1670KB ](774)
1169
28
Influence of temperature on tank pressurization system
MU Penggang, TONG Fei, PU Guangrong, MA Jian

2015 04 [74－78][Abstract](1167)[PDF:1989KB ](932)
1167
29
Analysis and test for limit speed of centrifugal impeller in liquid rocket engine
WANG Zhen1,TAN Yonghua2,HUANG Daoqiong1,XUAN Tong1

2017 05 [45－51][Abstract](1158)[PDF:1384KB ](572)
1158
30
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)
1142
31
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)
1141
32
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)
1134
33
Mass calculation of key assembly units in LH2/ LOX rocket engine based on visual interface
XUE wei, CAI Zhenyu, CAO Hongjuan, GE Qingming

2015 04 [61－66][Abstract](1128)[PDF:1245KB ](790)
1128
34
Research on feature extraction for fault monitoring of LOX/kerosene rocket engine
PU Xingxing1, WANG Jianshe2,GAO Yushan1, LI Chen1, ZHANG Xiaoping1

2017 06 [26－31][Abstract](1118)[PDF:577KB ](670)
1118
35
Research on high-power RF field reversed configuration plasma electromagnetic propulsion
SUN Xinfeng, WEN Xiaodong, ZHANG Tianping, GUO Ning, JIA Yanhui, WU Chenchen

2018 01 [44－52][Abstract](1114)[PDF:1796KB ](570)
1114
36
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)
1111
37
Research progress of flow-induced vibration of bellows
YAN Song1, TAN Yong-hua2, CHEN Jian-hua1

2014 02 [16－21][Abstract](1104)[PDF:1251KB ](644)
1104
38
Scheme of Chinese manned lunar rocket and its propulsion system
Zhang Xiaoping，Ding Fengnian，Ma Jie

2009 02 [1－6][Abstract](1097)[PDF:280KB ](607)
1097
39
Application of hybrid rocket engine in the fields of weapons and space launching
ZHAO Qing-hua1, WANG Li-li1, LIU Xin2

2014 06 [51－54][Abstract](1093)[PDF:327KB ](568)
1093
40
Study on pressurization of new generation launch vehicle
FAN Rui-xiang，TIAN Yu-rong，HUANG Bing

2012 04 [9－16][Abstract](1092)[PDF:486KB ](765)
1092
41
A rapid optimization design method for frame structure of double thrust chambers
HUO Shihui1, YUAN Junshe1, XU Xuejun1, YANG Sa2

2015 04 [55－60][Abstract](1090)[PDF:1581KB ](733)
1090
42
Investigation of thrust/drag property of scramjet
ZHAO Hong-liang, ZHANG Meng-zheng

2014 06 [41－45][Abstract](1088)[PDF:480KB ](714)
1088
43
Review on liquid film cooling of liquid rocket engine
TANG Liang, LI Ping, ZHOU Lixin

2020 01 [1－12][Abstract](1087)[PDF:3542KB ](556)
1087
44
Progress of regenerative cooling technology for scramjet
JIN Xuan,SHEN Chibing,WU Xianyu,YANG Jun,CHEN Yue

2016 05 [66－73][Abstract](1083)[PDF:4051KB ](799)
1083
45
Research on thermal protection coatings on body surface of Nb-Hf alloy thrust chamber
PAN Zhaoyi,CAI Gang,SONG Guoxin

2016 04 [68－73][Abstract](1082)[PDF:3098KB ](706)
1082
46
Machining technology research of cavitating venturi with deep tapered micro-hole
HE Weidong, ZHAN Haipeng, SHI Yong

2015 06 [68－72][Abstract](1078)[PDF:1186KB ](826)
1078
47
Modeling and simulation of start-up process of 60 t class LOX/methane liquid rocket engine
WANG Jun, ZHANG Wei-hong, SHI Wen-jing, ZHENG Da-yong

2013 05 [16－22][Abstract](1068)[PDF:2204KB ](538)
1068
48
Calculation and risk analysis of liquid hydrogen leakage and diffusion in launching site
DING Peng1, 2, CHEN Wei1, 2, REN Huizhong2, ZHOU Yu2

2018 04 [78－84][Abstract](1068)[PDF:918KB ](361)
1068
49
Analysis on research progress of mechanism of pyrotechnic valves abroad
YUAN Hongbin,HU Pan,WANG Zhiyong,SUN Lei

2016 02 [86－90][Abstract](1067)[PDF:1170KB ](684)
1067
50
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)
1065