Journal of Solid Rocket Technology 2009 Issue 1 Design and optimization of multi-stage solid launch rocket based on integrated stage concept

Design and optimization of multi-stage solid launch rocket based on integrated stage concept
GONG Chun-lin;GU Zhen-fang;ZHAO Ji-song;GU Liang-xian;GUO Lin-li;ZHANG Qi

..............page:1-5

A noncoplanar conic transfer arithmetic based on transfer time constraint
ZHANG Peng-yu;YANG Ming;WANG Zi-cai

..............page:6-10,19

Effect of shear fields on internal structure of the highly concentrated suspensions
GUO Ying;WANG Gang;XU Yuan-ze;YU Wei;ZHOU Chi-xing

..............page:70-73

Non-isothermal decomposition kinetics, specific heat capacity and adiabatic time-to-explosion of GNTO
XU Kang-zhen;ZHAO Feng-qi;YANG Ran;REN Ying-hui;MA Hai-xia;SONG Ji-rong

..............page:74-78

Study on preparation and catalytic properties of Co-B hollow nanospheres
SONG Dan;GUO Xiao-de;JIANG Wei;ZHANG Xiao-juan;LI Feng-sheng

..............page:79-82

Fracture criterion for mixed mode crack of composites based on the crack tip plastic zone
GAO Xin;WANG Han-gong;KANG Xing-wu

..............page:83-86

Optimization design of composite cylindrical lattice structure
HE Jing-xuan;HE Guo-qiang;HOU Xiao

..............page:87-89,99

Experimental investigation on bending property of 3D braided composites with stitching joint
LI Jia-lu;JIAO Ya-nan;SUN Qi-yong

..............page:90-94

Influence of homogenization method on fiber homogeneous effect and properties of C/C composite
GUO Ling-jun;LI He-jun;LI Ke-zhi;ZHANG Dong-sheng

..............page:95-99

Effect of content of boron oxide on structure and anti-oxidation property of SiC coating on C/C composites
SHI Xiao-hong;LI He-jun;ZENG Xie-rong;ZOU Ji-zhao

..............page:100-102,118

Effect of infiltration time on microstructure and mechanical properties of C/C-SiC composites
HUANG Pei-yu;XU Yong-dong;FAN Shang-wu;ZHANG Li-tong;CHENG Lai-fei

..............page:103-108

Synthesis and properties of PBO/SWNT composite fibers
WANG Feng;SONG Yuan-jun;HUANG Yu-dong;HU Na;LIN Hong;SUN De-zhi

..............page:109-113

Acousto-ultrasonic detection for interface defect between case and insulation of SRM
AI Chun-an;LIU Yu;CAI Kun

..............page:114-118

A terminal guidance law design applied to space-to-surface precision attack weapons
KANG Xing-wu;CHEN Gang;QIAO Yang;CHEN Shi-lu

..............page:11-14

Research on convergence speed of coning motion of wrap-around-fin rockets
ZHAO Liang-yu;YANG Shu-xing

..............page:15-19

Influence of support angle on air-driven separation process of low-shock separation device
ZHANG Xue-yuan;TANG Wen-yan

..............page:20-22,32

Research on numerical simulation of combustion gas jet under water
GAN Xiao-song;JIA You-jun;LU Chuan-jing;CAO Jia-yi

..............page:23-26

Comparison of fuel energy characteristics for supercavitation propulsion engine
GAO Ye;HE Zheng;LIU Pin-gan

..............page:27-32

Research on internal ballistics calculation uncertainty of solid rocket motors
ZOU Ru-ping;LI Xiao-bin;ZHANG Wei-hua

..............page:33-37,57

Numerical simulation and experimental study of deposition for ducted rockets
WANG De-quan;XIA Zhi-xun;HU Jian-xin;GUO Jian

..............page:38-42

Analysis on propellant crack deformation during prompt pressurization
ZHAO Ru-yan;YU Sheng-chun;LI Hao;WANG Guang

..............page:43-47

Numerical analysis on dynamic response characteristics of pintle-controlled solid rocket motor
LI Juan;WANG Zhan-li;ZHENG Kai;LI Jiang

..............page:48-52

Thermodynamic cycle analysis on solid propellant air-turbo-rocket
TU Qiu-ye;DING Chao-xia;CHEN Yu-chun;CAI Yuan-hu

..............page:53-57

Aerodynamic optimization research for contour of ramjet assisted projectile inlet
WANG Xiao-rong;JIANG Gen-zhu;ZHOU Chang-sheng

..............page:58-60,82

Analysis and comparison of analytical and numerical solutions of flow field in solid rocket motors with tapered sidewalls
WANG Ge;DU Gui-xian;FANG Lei;ZHANG Hong-yan

..............page:61-66

Damage and shock sensitivity change of NEPE propellant under temperature changing conditions
ZHENG Xue;LI Jing-ming;ZHAO Xiao-bin

..............page:67-69