Spacecraft Recovery & Remote Sensing, Volume. 46, Issue 1, 1(2025)

Multi Objective Optimization and Design of Reinstalling Airdrop Buffer System

Haoyang WANG1,2, Chen WANG1,2、*, Chaoyu LU1,2, and Jinbao CHEN1,2
Author Affiliations
  • 1Laboratory of Aerospace Entry, Descent and Landing Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
  • 2Academy of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
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    References(7)

    [4] [4] TAYL A P. Design Optimization of the Beagle ⅡMars Ler Airbags Through Explicit Finite Element Analysis[C]15th Aerodynamic Decelerat Systems Technology Conference. Toulouse, France: AIAA, 2000: 1528. DOI: 10.25146.19991743.

    [8] [8] VASSILAKOS G J, STEGALL D E, HARDY R C, et al. ion Crew Module Ling System Simulation Verification[C]2011 Aerospace Conference. Big Sky, MT, USA: IEEE, 2011: 123. DOI: 10.1109AERO.2011.5747623.

    [10] [10] WELCH J. CEV Airbag Ling System Modeling[C]19th AIAA Aerodynamic Decelerat Systems Technology Conference Seminar. Williamsburg, VA: AIAA, 2007: AIAA 20072533. DOI: 10.25146.20072533.

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    Haoyang WANG, Chen WANG, Chaoyu LU, Jinbao CHEN. Multi Objective Optimization and Design of Reinstalling Airdrop Buffer System[J]. Spacecraft Recovery & Remote Sensing, 2025, 46(1): 1

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    Paper Information

    Category:

    Received: Sep. 11, 2024

    Accepted: --

    Published Online: Apr. 2, 2025

    The Author Email: Chen WANG (nuaawangchen@nuaa.edu.cn)

    DOI:10.3969/j.issn.1009-8518.2025.01.001

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