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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](3281)[PDF:1282KB ](2108)
3281
2
Development and application of Hall electric propulsion technology
KANG Xiaolu1, 2, HANG Guanrong1, 2，ZHU Zhichun1, 2

2017 01 [8－17][Abstract](2812)[PDF:2378KB ](2405)
2812
3
Research progress on ignition of HAN-based green propellant
WANG Xinqiang,DENG Kangqing,LI Hongxu,YU Xiaobo

2017 02 [72－76][Abstract](2436)[PDF:330KB ](1775)
2436
4
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](2365)[PDF:1805KB ](2004)
2365
5
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](2212)[PDF:413KB ](1558)
2212
6
Development Status and Trends of Liquid Propellant

2004年01期 [1－6][Abstract](2039)[PDF:419KB ](1231)
2039
7
Review on technology development of solid rocket motor
MA Shuai, GUO Jianxin, ZHOU Lei, ZHU Zihuan

2023 02 [1－14][Abstract](1973)[PDF:6382KB ](959)
1973
8
Integration design system for turbo pump in rocket engine
ZHANG Chenxi1, MA Xiaodan2

2015 04 [79－83][Abstract](1939)[PDF:1572KB ](1294)
1939
9
Thrust Calculation of Liquid Rocket Engine post Flight
Bu Nailan

2004年05期 [18－21][Abstract](1931)[PDF:36KB ](1000)
1931
10
Application of additive manufacturing technology in liquid rocket engine
ZUO Wei, SONG Menghua, YANG Huanqing, CHEN Xinhong

2018 02 [55－65][Abstract](1910)[PDF:32055KB ](1309)
1910
11
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](1873)[PDF:276KB ](1146)
1873
12
System configuration of LOX/methane rocket engine with dual-bell nozzle
ZHANG Wei-hong, SHI Wen-jing, ZHENG Meng-wei

2013 03 [9－14][Abstract](1870)[PDF:2207KB ](690)
1870
13
Digital measurement system for cryogenic liquid level
DUAN Wenhao, ZHANG Jia, WANG Hongyue

2017 03 [79－82][Abstract](1855)[PDF:1004KB ](1571)
1855
14
esearch on plume flow of space thrusters
GUO Jing, KONG Fan-chao, HU Xu-kun

2014 06 [46－50][Abstract](1853)[PDF:1373KB ](1684)
1853
15
Application status and key technology of bipropellant blowdown propulsion systems
YANG Jun,HE Yongying,LIAN Renzhi,YANG Fushu

2016 04 [21－25][Abstract](1787)[PDF:3119KB ](1130)
1787
16
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](1747)[PDF:1796KB ](943)
1747
17
Investigation of thrust/drag property of scramjet
ZHAO Hong-liang, ZHANG Meng-zheng

2014 06 [41－45][Abstract](1738)[PDF:480KB ](1062)
1738
18
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](1718)[PDF:1384KB ](921)
1718
19
Application of AMESim in dynamic characteristic simulation of liquid rocket engine system
PAN Hui, ZHANG Li-hui

2011 03 [6－11][Abstract](1710)[PDF:454KB ](1576)
1710
20
Calculation of fuel gas thermodynamic parameters and transport coefficients for oxygen/kerosene engine
WANG Xin, ZOU Yanghui

2017 04 [34－40][Abstract](1708)[PDF:704KB ](1222)
1708
21
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](1681)[PDF:327KB ](923)
1681
22
Research progress of nitrous oxide propulsion technology
SONG Chang-qing, XU Wan-wu, ZHANG Jia-qi, CHEN Jian

2014 02 [7－15][Abstract](1678)[PDF:2348KB ](1178)
1678
23
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](1668)[PDF:1245KB ](1149)
1668
24
Progress of optimization for bipropellant uniform propulsion system
YUAN Lei, WANG Shen, LIU Tao, LIAN Ren-zhi

2014 06 [7－10][Abstract](1666)[PDF:1628KB ](1271)
1666
25
Simulation of gas pressure inside high pressure vessel of pressure-fed propellant feed system
WANG Kun1, LI Chun-fei2, DONG Yuan2

2013 02 [79－82][Abstract](1660)[PDF:184KB ](1035)
1660
26
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](1658)[PDF:1019KB ](1452)
1658
27
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](1645)[PDF:911KB ](1092)
1645
28
Ferroelectric emission ：hodes for 1 OW lCcathod Ior low-power electric propulsion
Sheng Zhaoxuanl，Feng Yujun2,Xu Zhuo2，Sun Xinlil

2008 02 [37－40][Abstract](1636)[PDF:243KB ](980)
1636
29
Preliminary design for composite thrust frame of liquid rocket engine
MU Penggang, LI Binchao, DU Dahua, DENG Changhua

2017 03 [35－41][Abstract](1613)[PDF:1206KB ](1466)
1613
30
Design philosophy of high-pressure & high-lift centrifugal pump for solid-liquid phase mediums
YU Hai-li1, ZHANG Rui1, LIU Hai-li1, Lü Zhi-quan2, WU Yu-zhen1

2015 02 [70－74][Abstract](1602)[PDF:1611KB ](1071)
1602
31
Study on the LOX／methane rocket engine power cycles
Zhang Xiaoping，Li Chunhong，Ma Dongying

2009 04 [14－20][Abstract](1589)[PDF:407KB ](965)
1589
32
Study of inducers for low-NPSHr high-speed pumps
HOU Jie, YU Hai-li, YANG Min

2014 06 [16－20][Abstract](1578)[PDF:1226KB ](1011)
1578
33
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](1572)[PDF:918KB ](683)
1572
34
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](1541)[PDF:1581KB ](1096)
1541
35
Scheme of Chinese manned lunar rocket and its propulsion system
Zhang Xiaoping，Ding Fengnian，Ma Jie

2009 02 [1－6][Abstract](1523)[PDF:280KB ](945)
1523
36
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](1522)[PDF:809KB ](1054)
1522
37
Application of RBCC and TBCC engines to RLVs
Chen Hong1，He Guoqiang2

2008 03 [39－43][Abstract](1521)[PDF:267KB ](1422)
1521
38
Review on liquid film cooling of liquid rocket engine
TANG Liang, LI Ping, ZHOU Lixin

2020 01 [1－12][Abstract](1521)[PDF:3542KB ](929)
1521
39
Influence of temperature on tank pressurization system
MU Penggang, TONG Fei, PU Guangrong, MA Jian

2015 04 [74－78][Abstract](1510)[PDF:1989KB ](1302)
1510
40
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](1504)[PDF:2204KB ](891)
1504
41
Research on a novel bipropellant for spacecrafts
HUANG Ji-qing, BAO Shi-guo, LIU Han-lin, LIU Jiang-qiang

2013 03 [67－71][Abstract](1494)[PDF:325KB ](1027)
1494
42
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](1494)[PDF:351KB ](1268)
1494
43
Unsteady numerical simulation of the inlet with a bleed slot in oscillating flow
Wang Mingkun, Dong Jinzhong, Hu Xueguang

2009 06 [5－8][Abstract](1488)[PDF:306KB ](508)
1488
44
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](1482)[PDF:2214KB ](988)
1482
45
Influence of RBCC rocket on resisting backpressure ability of straight-expanded flowpath
LIU Xiaowei, LIU Hao, ZHANG Mengzheng

2015 06 [7－10][Abstract](1478)[PDF:1591KB ](878)
1478
46
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](1477)[PDF:396KB ](1207)
1477
47
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](1475)[PDF:1434KB ](1043)
1475
48
Influence of nozzle inlet Mach number on performance of scramjet nozzle
WEN Ke, LI Xu-chang, MA Cen-rui, MA Hai-ying, SONG Ya-fei

2011 03 [18－21][Abstract](1471)[PDF:312KB ](673)
1471
49
Comparative study on electric pump and pressure-fed propulsion systems
LIU Changbo

2017 02 [32－39][Abstract](1465)[PDF:451KB ](1483)
1465
50
Research on ground test technology for swing status of LOX/LH2 rocket engine
XIA Wei，CHEN Shi-zhe，WANG Zhan-lin，ZHU Zi-yong

2015 01 [105－111][Abstract](1463)[PDF:2675KB ](670)
1463