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An Efficient and Effective Light Gas Gun Design for Millimeter-scale Hypervelocity TestingThis paper serves to document a design for a light gas gun that was used for 3 decades at NASA’s Langley Research Center. By adapting readily-available equipment and supplies, this apparatus was capable of accelerating projectiles at up to 9 kilometers per second (when new). The lack of a projectile-carrying sabot sacrifices some adaptability in projectile size, but results in a design that can be cleaned and cycled with far less labor input. Overall limitation on the projectile impact energies attainable effectively limit the applications to assessing the relatively thin shields employed for robotic spacecraft (less useful for those used for manned missions). The original gun has been decommissioned, but it is believed that this design has application for robotic spacecraft shield testing in the modern world, allowing cost-effective generation of larger sample sizes than with conventional sabot-based light gas guns.
Document ID
20230017078
Acquisition Source
Goddard Space Flight Center
Document Type
Poster
Authors
Scott Hull
(Goddard Space Flight Center Greenbelt, United States)
Mark Kulick
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Donald Humes
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 21, 2023
Subject Category
Engineering (General)
Structural Mechanics
Meeting Information
Meeting: 2nd International Orbital Debris Conference (IOC II)
Location: Houston, TX
Country: US
Start Date: December 4, 2023
End Date: December 7, 2023
Sponsors: Lunar and Planetary Institute
Funding Number(s)
WBS: 385616.07.02.02
CONTRACT_GRANT: 80LARC23DA003
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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