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Essentials of configuration design of HALE solar-powered UAVs
ZHANG Jian, ZHANG Dehu
doi: 10.7527/S1000-6893.2016.0244
2016, (S1): 1-7.
PDF [ 7520 K ]( 2431 ) HTML
Key technologies and solutions for large extensible door of re-entry space vehicle
LI Baojiang, SHAO Jiming, WANG Changhuan, HUANG Peng
doi: 10.7527/S1000-6893.2016.0243
2016, (S1): 8-15.
PDF [ 6828 K ]( 1083 ) HTML
Energy balance modeling for solar powered aircrafts
ZHANG Dehu, ZHANG Jian, LI Junfu
doi: 10.7527/S1000-6893.2016.0236
2016, (S1): 16-23.
PDF [ 2742 K ]( 1053 ) HTML
An aerodynamic identification and correction method for vehicle in release separation
ZENG Xiaobin, PENG Jun, YUE Chuan
doi: 10.7527/S1000-6893.2016.0226
2016, (S1): 24-31.
PDF [ 2673 K ]( 859 ) HTML
Test and analysis of natural modal characteristics of a wing model with thermal effect
TAN Guanghui, LI Qiuyan, DENG Jun
doi: 10.7527/S1000-6893.2016.0148
2016, (S1): 32-37.
PDF [ 2308 K ]( 2169 ) HTML
Hypersonic aircraft's carbon-based nose ablation shape calculation
CHEN Zifa, ZHANG Xiaochen, WANG Zhenfeng, XU Yun, XU Xiaoliang
doi: 10.7527/S1000-6893.2016.0161
2016, (S1): 38-45.
PDF [ 2980 K ]( 1148 ) HTML
Cabin environment design and application for hypersonic vehicle
PAN Lixin, YANG Jiayong, WANG Man, KONG Bin
doi: 10.7527/S1000-6893.2016.0160
2016, (S1): 46-52.
PDF [ 2588 K ]( 892 ) HTML
Analysis and design of leading edge using metallic thermal protection system
WANG Man, YANG Jiayong, HE Erfeng, TU Bing
doi: 10.7527/S1000-6893.2016.0176
2016, (S1): 53-58.
PDF [ 2258 K ]( 885 ) HTML
Properties of high-temperature heat pipe and its experimental
NIU Tao, ZHANG Yanling, HOU Hongliang, WANG Yaoqi, HE Duo
doi: 10.7527/S1000-6893.2016.0165
2016, (S1): 59-65.
PDF [ 2709 K ]( 937 ) HTML
Thermoelectric coupling calculation method for aircraft thermal antenna
ZHANG Xiaochen, LIN Chaoguang, WANG Zhenfeng, YU Mingxing, TAN Heping
doi: 10.7527/S1000-6893.2016.0193
2016, (S1): 66-72.
PDF [ 2565 K ]( 607 ) HTML
Thermal test technique of complex structure of hypersonic aircraft
LI Xiang, FU Bo
doi: 10.7527/S1000-6893.2016.0208
2016, (S1): 73-79.
PDF [ 2675 K ]( 1016 ) HTML
Analysis and control of nonlinear loss of stability for longitudinal flight dynamics of hypersonic vehicle with high angle of attack
SU Erlong, LUO Jianjun, MIN Changwan
doi: 10.7527/S1000-6893.2016.0172
2016, (S1): 80-90.
PDF [ 3792 K ]( 1129 ) HTML
Design of redundant fault-tolerant navigation system for near space UAV
WU Yongliang, CAI Ya'nan, BAOYIN Hexi, XIONG Lichuan, LIU Shengchuan
doi: 10.7527/S1000-6893.2016.0171
2016, (S1): 91-98.
PDF [ 2770 K ]( 863 ) HTML
Trajectory design for terminal area energy management of suborbital reusable launch vehicle
ZANG Xiheng, HU Yongtai
doi: 10.7527/S1000-6893.2016.0170
2016, (S1): 99-105.
PDF [ 2575 K ]( 620 ) HTML
Design and simulation of configurations for aerodynamic surfaces/RCS blended control system
LU Cunkan, HU Yongtai
doi: 10.7527/S1000-6983.2016.0167
2016, (S1): 106-111.
PDF [ 2208 K ]( 724 ) HTML
Unsteady combustion process in multi-cavity combustor at low Mach number condition
WANG Lu, GAO Liangjie, QIAN Zhansen, ZHAO Yong
doi: 10.7527/S1000-6893.2016.0149
2016, (S1): 112-118.
PDF [ 2656 K ]( 1618 ) HTML
Key technology for pre-cooler in near space vehicle propulsion system
LYU Duo, LU Haiying, ZHOU Jianjun, SHANG Shoutang, YU Xiao
doi: 10.7527/S1000-6893.2016.0164
2016, (S1): 119-126.
PDF [ 2802 K ]( 1198 ) HTML
Payload platform of near space vehicle information system
YAN Xiao, TANG Bo, ZHANG Tianhong, QIN Kaiyu
doi: 10.7527/S1000-6893.2016.0181
2016, (S1): 127-133.
PDF [ 2623 K ]( 1566 ) HTML
Path analysis and network performance simulation based on near space vehicle
JIN Chao, QIU Qiming, PENG Wenpan
doi: 10.7527/S1000-6893.2016.0147
2016, (S1): 134-138.
PDF [ 2052 K ]( 876 ) HTML
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