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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. 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 (as opposed to 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
20220013697
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Scott Hull
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Mark Kulick
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Don Humes
(Langley Research Center (Retired) Hampton, Virginia, United States)
Date Acquired
September 7, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Hypervelocity Impact Symposium (HVIS) 2022
Location: Alexandria, VA
Country: US
Start Date: September 18, 2022
End Date: September 22, 2022
Sponsors: Johns Hopkins University Applied Physics Laboratory
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Hypervelocity
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