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2023, (23): 0-.
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A review of reusable launch vehicle technology development
Weimin BAO
doi: 10.7527/S1000-6893.2023.29555
2023, (23): 629555-629555.
PDF [ 1049 K ]( 1089 ) HTML
Prospects for fatigue durability and reliability of reusable launch vehicle structures
Mengqi GU, Jiacai ZHU, Wanlin GUO, Song XUE
doi: 10.7527/S1000-6893.2023.28299
2023, (23): 628299-628299.
PDF [ 7167 K ]( 515 ) HTML
Guidance and control for powered descent and landing of launch vehicles: Overview and outlook
Linkun HE, Wenchao XUE, Ran ZHANG, Huifeng LI
doi: 10.7527/S1000-6893.2023.28462
2023, (23): 628462-628462.
PDF [ 4051 K ]( 288 ) HTML
Review and prospect of model-based fault diagnosis technology for liquid rocket engines
Zehao CHEN, Hui CHEN, Yushan GAO, Hang ZHANG
doi: 10.7527/S1000-6893.2023.29016
2023, (23): 629016-629016.
PDF [ 2298 K ]( 310 ) HTML
Behavior of cryogenic propellant in return stage of reusable launch vehicle
Yi RONG, Hui LIU, Ziwen YU, Pingping ZHU, Yue PENG, Jiahui YU
doi: 10.7527/S1000-6893.2023.29563
2023, (23): 629563-629563.
PDF [ 4797 K ]( 202 ) HTML
Powered deceleration guidance method based on gravity-turn analytical solutions
Zhi ZHANG, Han YUAN, Wanqing ZHANG
doi: 10.7527/S1000-6893.2023.28483
2023, (23): 628483-628483.
PDF [ 4431 K ]( 178 ) HTML
Reconfigurability and autonomous reconfiguration methods of spacecraft
Yuanyuan TU, Dayi WANG, Xiangyan ZHANG, Jiaxing LI, Xiaofeng HUANG
doi: 10.7527/S1000-6893.2023.28855
2023, (23): 628855-628855.
PDF [ 1350 K ]( 39 ) HTML
Reliable communication technologies of reusable launch vehicles in cooperation with satellite during re-entry
Xiaoping LI, Min YANG, Bo YAO, Yanming LIU, Lei SHI, Haoyan LIU, Chengguang LI
doi: 10.7527/S1000-6893.2023.28906
2023, (23): 628906-628906.
PDF [ 9277 K ]( 83 ) HTML
Combined disturbance compensation guidance for powered descent in atmosphere
Xinglun CHEN, Ran ZHANG, Xiaoyan ZHANG
doi: 10.7527/S1000-6893.2022.28465
2023, (23): 628465-628465.
PDF [ 5490 K ]( 113 ) HTML
Full flight profile prescribed performance control for vertical take-off and vertical landing reusable launch vehicle
Liang ZHANG, Danyu LI, Naigang CUI, Yuan LI
doi: 10.7527/S1000-6893.2022.28103
2023, (23): 628103-628103.
PDF [ 3874 K ]( 157 ) HTML
Reusable technology of air⁃launched launch vehicle
Yan LYU, Lin LIU, Guangyong ZHANG, Lei LIANG, Xuesheng ZHENG
doi: 10.7527/S1000-6893.2022.28083
2023, (23): 628083-628083.
PDF [ 2453 K ]( 146 ) HTML
Theoretical and experimental on two-phase flow mechanism of low-temperature high-speed hydrodynamic mechanical seal
Guoyuan ZHANG, Xukang LI, Weigang ZHAO, Yangyang ZHAO, Junqian WANG
doi: 10.7527/S1000-6893.2022.28229
2023, (23): 628229-628229.
PDF [ 4090 K ]( 125 ) HTML
Wind tunnel test of fluctuating pressure on aeroelastic scaled model of hammerhead launch vehicle
Chang LIU, Yunlong ZHANG, Zhijiang YAN, Lei ZHAO, Chen JI
doi: 10.7527/S1000-6893.2023.28384
2023, (23): 128384-128384.
PDF [ 7871 K ]( 106 ) HTML
Wide-speed aerodynamic layout adopting waverider-delta wing
Shusheng CHEN, Zhaokang ZHANG, Jinping LI, Cong FENG, Zhenghong GAO
doi: 10.7527/S1000-6893.2023.28441
2023, (23): 128441-128441.
PDF [ 6335 K ]( 229 ) HTML
Equivalent calculation method of irradiance distribution of spectrum simulator array
Xinxin LI, Binwen WANG, Xiaoxiao ZHANG, Linhua CONG, Jingtao WU
doi: 10.7527/S1000-6893.2023.28493
2023, (23): 228493-228493.
PDF [ 5130 K ]( 59 ) HTML
Parameter calibration and reliability analysis of an aero-engine rotor based on multi-source heterogeneous information
Lechang YANG, Chenxing WANG
doi: 10.7527/S1000-6893.2023.28575
2023, (23): 228575-228575.
PDF [ 3144 K ]( 104 ) HTML
Prediction method of ablation and thermal response for a thermal protection coating with silicone rubber
Shengbo SHI, Bao LEI, Yuntian ZHANG, Li HU, Maoyuan LI, Jun LIANG
doi: 10.7527/S1000-6893.2022.28141
2023, (23): 428141-428141.
PDF [ 4120 K ]( 127 ) HTML
In⁃situ explosion limit of thermal runaway gas explosion in cyclic aging lithium⁃ion batteries: Experimental analysis
Juan YANG, Jianghao NIU, Qingsong ZHANG
doi: 10.7527/S1000-6893.2023.28529
2023, (23): 428529-428529.
PDF [ 2400 K ]( 88 ) HTML
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