Investigation of the application of airbag technology to provide a softlanding capability for military heavy airdrop

Author:

Taylor Anthony1,Benney Richard2,Bagdonovich Brian2

Affiliation:

1. Irvin Aerospace, Inc., Santa Ana, CA

2. U.S. Army, Soldier and Biological Chemical Command, Natick, MA

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. Brown, G. Haggard, R. Benney, R. "Parachute Retraction, Soft-landing SystemsusingPneumatic MuscleActuators"AIAA-2000-4308

2. Taylor,A.P. "DesignOptimizationoftheBeagle IIMarsLanderAirbagsThrough Explicit Finite ElementAnalysis",AIAApaper 99-1743

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2. Parameterized Design and Dynamic Analysis of a Reusable Launch Vehicle Landing System with Semi-Active Control;Symmetry;2020-09-22

3. Simulation of the Landing Dynamics of a Guided Airdrop System;AIAA Aviation 2019 Forum;2019-06-15

4. Research on Cushion Characteristics of Self-Inflating Buffering Airbag;Applied Mechanics and Materials;2014-01

5. FLOATSTAB - A Tool for the Rapid Analysis of Flotation Stability Following Water Landing;18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2005-05-23

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