With more than 1 trillion artificial objects smaller than 1 μm in low and geostationary Earth orbit, space assets are subject to the constant threat of space debris impact. These collisions occur at hypervelocity or speeds greater than 3 km/s. In order to characterize material behavior under this extreme event as well as study next-generation materials for space exploration, this paper presents a unique two-stage light-gas gun capable of replicating hypervelocity impacts. While a limited number of these types of facilities exist, they typically are extremely large and can be costly and dangerous to operate. The design presented in this paper is novel in two distinct ways. First, it does not use a form of combustion in the first stage. The projectile is accelerated from a pressure differential using air and inert gases (or purely inert gases), firing a projectile in a nominal range of 1–4 km/s. Second, the design is modular in that the first stage sits on a track sled and can be pulled back and used in itself to study lower speed impacts without any further modifications, with the first stage piston as the impactor. The modularity of the instrument allows the ability to investigate three orders of magnitude of impact velocities or between 101 and 103 m/s in a single, relatively small, cost effective instrument.
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February 2018
Research Article|
February 13 2018
Compressed gas combined single- and two-stage light-gas gun
L. E. Lamberson;
L. E. Lamberson
a)
Mechanical Engineering and Mechanics, Drexel University
, Philadelphia, Pennsylvania 19104, USA
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P. A. Boettcher
P. A. Boettcher
Mechanical Engineering and Mechanics, Drexel University
, Philadelphia, Pennsylvania 19104, USA
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Rev. Sci. Instrum. 89, 023903 (2018)
Article history
Received:
August 19 2017
Accepted:
January 04 2018
Citation
L. E. Lamberson, P. A. Boettcher; Compressed gas combined single- and two-stage light-gas gun. Rev. Sci. Instrum. 1 February 2018; 89 (2): 023903. https://doi.org/10.1063/1.5000912
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