Down-bore two-laser heterodyne velocimetry of an implosion-driven hypervelocity launcher

The implosion-driven launcher uses explosives to shock-compress helium, driving well-characterized projectiles to velocities exceeding 10 km/s. The masses of projectiles range between 0.1 – 15 g, and the design shows excellent scalability, reaching similar velocities across different projectile size...

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Bibliographic Details
Main Authors: Hildebrand, Myles, Huneault, Justin, Loiseau, Jason, Higgins, Andrew J.
Format: Conference Proceeding
Language:English
Subjects:
Ballistics
Explosive compacting
Helium
Hypervelocity
Hypervelocity launchers
Lasers
Projectiles
Velocimetry
Velocity
Velocity measurement
Videography
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Summary:The implosion-driven launcher uses explosives to shock-compress helium, driving well-characterized projectiles to velocities exceeding 10 km/s. The masses of projectiles range between 0.1 – 15 g, and the design shows excellent scalability, reaching similar velocities across different projectile sizes. In the past, velocity measurements have been limited to muzzle velocity obtained via a high-speed videography upon the projectile exiting the launch tube. Recently, Photon Doppler Velocimetry (PDV) has demonstrated the ability to continuously measure in-bore velocity, even in the presence of significant blow-by of high temperature helium propellant past the projectile. While a single laser system sampled at 40 GS/s with a 13 GHz detector/scope bandwidth is limited to 8 km/s, a two-laser PDV system is developed that uses two lasers operating near 1550 nm to provide velocity measurement capabilities up to 16 km/s with the same bandwidth and sampling rate. The two-laser PDV system is used to obtain a continuous velocity history of the projectile throughout the entire launch cycle. These internal ballistics trajectories are used to compare different advanced concepts aimed at increasing the projectile velocity to well beyond 10 km/s.
ISSN:0094-243X
1551-7616
DOI:10.1063/1.4971749