Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 5, 1(2024)

Research on the Impact Characteristics of Re-entry Capsule with Airbags under Wave Conditions

Jiapeng HAN1,2, Shiqing WU2,3, Yang ZHANG1,2、*, Jiangli LEI2,3, Wei HUANG2,3, and Meifang ZHU2,3
Author Affiliations
  • 1College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 2Laboratory of Aerospace Entry, Descent and Landing Technology, CASC, Beijing 100094, China
  • 3Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
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    References(5)

    [1] [1] KROSS D A, KEIFLING L A, MURPHY N C, et al. Space Shuttle Solid Rocket Booster Initial Water Impact Loads Dynamicsanalysis, Tests, Flight Experience[C]American Institute of Aeronautics Astronautics 24th Structures, Structural Dynamics Materials Conference, May 0204, 1983, Lake Tahoe, NV, USA.

    [4] [4] WANG J T, LYLE K H. Simulating Space Capsule Water Ling with Explicit Finite Element Method[C]48th AIAAASMEEAHS Structures, Structural Dynamics, Materials Conference, April 2326, 2007, Honolulu, Hawaii, USA.

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    Jiapeng HAN, Shiqing WU, Yang ZHANG, Jiangli LEI, Wei HUANG, Meifang ZHU. Research on the Impact Characteristics of Re-entry Capsule with Airbags under Wave Conditions[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(5): 1

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    Paper Information

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    Received: Jan. 9, 2024

    Accepted: --

    Published Online: Nov. 13, 2024

    The Author Email: ZHANG Yang (zhy@nuaa.edu.cn)

    DOI:10.3969/j.issn.1009-8518.2024.05.001

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