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The Hanging Scheme and Simulation Analysis for the Tail Cabin of Launch Vehicle based on Aerial Recovery
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Zhenglu ZHENG1, Xiaowei WANG1, Qiong WU2, Yi SUI3, Zhenliang XU1
Missiles and Space Vehicles | 2024, 47(2) : 11 - 16
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Missiles and Space Vehicles | 2024, 47(2): 11-16
• Launch Vehicle and Missile •
The Hanging Scheme and Simulation Analysis for the Tail Cabin of Launch Vehicle based on Aerial Recovery
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Zhenglu ZHENG1, Xiaowei WANG1, Qiong WU2, Yi SUI3, Zhenliang XU1
Affiliations
  • 1China Academy of Launch Vehicle Technology,Beijing,100076
  • 2Beihang University,Beijing,100191
  • 3Beijing Institute of Space Mechanics & Electricity,Beijing,100094
Published: 2024-04-25 doi: 10.7654/j.issn.2097-1974.20240203
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The hanging process is one of the key links in the Mid-Air retrieval of launch vehicle. According to the whole process of the launch vehicle tail cabin hanging in the air, the design of the hanging device based on the helicopter as the recovery platform is carried out. The hanging device includes tension sensor, load shedding device, overload protection device and the actuator in the end of the hanging device. Parafoil and parachute eject from the bottom of the tail cabin of launch vehicle. The hanging device can realize the hanging operation of the retrieval by hanging attached apex drogue on the top of parafoil. Through the simulation analysis of the hanging process, it can be seen that when the weight of the retrieval increases, the overload increases significantly. When the parachute retraction time increases, the load reduction effect is obvious

launch vehicle  /  aerial recovery  /  hanging device  /  parafoil  /  load shedding
Zhenglu ZHENG, Xiaowei WANG, Qiong WU, Yi SUI, Zhenliang XU. The Hanging Scheme and Simulation Analysis for the Tail Cabin of Launch Vehicle based on Aerial Recovery[J]. Missiles and Space Vehicles, 2024 , 47 (2) : 11 -16 . DOI: 10.7654/j.issn.2097-1974.20240203
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Year 2024 volume 47 Issue 2
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Article Info
doi: 10.7654/j.issn.2097-1974.20240203
  • Receive Date：2021-07-28
  • Online Date：2025-07-04
  • Published：2024-04-25
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  • Received：2021-07-28
  • Revised：2021-10-23
Affiliations
    1China Academy of Launch Vehicle Technology,Beijing,100076
    2Beihang University,Beijing,100191
    3Beijing Institute of Space Mechanics & Electricity,Beijing,100094
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Citations
表12种不同金属材料的力学参数
科
Family		 属数
Number of
genus		 种数
Number of
species		 占总种数比例
Percentage of
total species (%)		 属
Genus		 种数
Number of
species		 占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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