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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](3157)[PDF:1282KB ](1979)
3157
2
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)
2647
3
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)
2313
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](2242)[PDF:1805KB ](1869)
2242
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](2115)[PDF:413KB ](1430)
2115
6
Development Status and Trends of Liquid Propellant

2004年01期 [1－6][Abstract](1987)[PDF:419KB ](1106)
1987
7
Thrust Calculation of Liquid Rocket Engine post Flight
Bu Nailan

2004年05期 [18－21][Abstract](1909)[PDF:36KB ](891)
1909
8
Integration design system for turbo pump in rocket engine
ZHANG Chenxi1, MA Xiaodan2

2015 04 [79－83][Abstract](1807)[PDF:1572KB ](1171)
1807
9
Review on technology development of solid rocket motor
MA Shuai, GUO Jianxin, ZHOU Lei, ZHU Zihuan

2023 02 [1－14][Abstract](1772)[PDF:6382KB ](809)
1772
10
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](1744)[PDF:276KB ](1016)
1744
11
Digital measurement system for cryogenic liquid level
DUAN Wenhao, ZHANG Jia, WANG Hongyue

2017 03 [79－82][Abstract](1742)[PDF:1004KB ](1441)
1742
12
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)
1735
13
Application status and key technology of bipropellant blowdown propulsion systems
YANG Jun,HE Yongying,LIAN Renzhi,YANG Fushu

2016 04 [21－25][Abstract](1686)[PDF:3119KB ](999)
1686
14
esearch on plume flow of space thrusters
GUO Jing, KONG Fan-chao, HU Xu-kun

2014 06 [46－50][Abstract](1686)[PDF:1373KB ](1544)
1686
15
Investigation of thrust/drag property of scramjet
ZHAO Hong-liang, ZHANG Meng-zheng

2014 06 [41－45][Abstract](1624)[PDF:480KB ](944)
1624
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](1624)[PDF:1796KB ](816)
1624
17
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)
1606
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](1605)[PDF:1384KB ](797)
1605
19
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)
1602
20
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)
1601
21
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](1564)[PDF:1245KB ](1026)
1564
22
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)
1562
23
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)
1553
24
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](1539)[PDF:184KB ](912)
1539
25
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](1534)[PDF:327KB ](809)
1534
26
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)
1518
27
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](1509)[PDF:243KB ](789)
1509
28
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](1505)[PDF:911KB ](975)
1505
29
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](1481)[PDF:1611KB ](956)
1481
30
Study on the LOX／methane rocket engine power cycles
Zhang Xiaoping，Li Chunhong，Ma Dongying

2009 04 [14－20][Abstract](1472)[PDF:407KB ](842)
1472
31
Scheme of Chinese manned lunar rocket and its propulsion system
Zhang Xiaoping，Ding Fengnian，Ma Jie

2009 02 [1－6][Abstract](1466)[PDF:280KB ](834)
1466
32
Study of inducers for low-NPSHr high-speed pumps
HOU Jie, YU Hai-li, YANG Min

2014 06 [16－20][Abstract](1457)[PDF:1226KB ](888)
1457
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](1455)[PDF:918KB ](555)
1455
34
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](1444)[PDF:2214KB ](870)
1444
35
Application of RBCC and TBCC engines to RLVs
Chen Hong1，He Guoqiang2

2008 03 [39－43][Abstract](1444)[PDF:267KB ](1302)
1444
36
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](1428)[PDF:1581KB ](976)
1428
37
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)
1427
38
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](1422)[PDF:809KB ](941)
1422
39
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](1413)[PDF:1434KB ](923)
1413
40
Review on liquid film cooling of liquid rocket engine
TANG Liang, LI Ping, ZHOU Lixin

2020 01 [1－12][Abstract](1403)[PDF:3542KB ](818)
1403
41
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](1402)[PDF:2204KB ](767)
1402
42
Research on a novel bipropellant for spacecrafts
HUANG Ji-qing, BAO Shi-guo, LIU Han-lin, LIU Jiang-qiang

2013 03 [67－71][Abstract](1398)[PDF:325KB ](898)
1398
43
Influence of temperature on tank pressurization system
MU Penggang, TONG Fei, PU Guangrong, MA Jian

2015 04 [74－78][Abstract](1397)[PDF:1989KB ](1179)
1397
44
Influence of RBCC rocket on resisting backpressure ability of straight-expanded flowpath
LIU Xiaowei, LIU Hao, ZHANG Mengzheng

2015 06 [7－10][Abstract](1376)[PDF:1591KB ](813)
1376
45
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)
1375
46
Lander descent engine and assumption of Chinese LMDE
LEI Juan-ping, MA Jie, LIU Chang-bo

2010 05 [1－6][Abstract](1373)[PDF:339KB ](635)
1373
47
Unsteady numerical simulation of the inlet with a bleed slot in oscillating flow
Wang Mingkun, Dong Jinzhong, Hu Xueguang

2009 06 [5－8][Abstract](1369)[PDF:306KB ](446)
1369
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](1365)[PDF:312KB ](613)
1365
49
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](1362)[PDF:1670KB ](989)
1362
50
Comparative study on electric pump and pressure-fed propulsion systems
LIU Changbo

2017 02 [32－39][Abstract](1361)[PDF:451KB ](1351)
1361