Use of Electromagnetic Coil Launcher to Increase Muzzle Velocity of Conventional Cannons.
Abstract
This paper describes the design and operation of an experimental hybrid cannon consisting of a 60-mm bore gas cannon using standard propellant and a traveling-wave induction accelerator. The projectile, consisting of an aluminum cylinder weighing 120 grams, is initially brought up to a speed of 600 m/s in the gas cannon. The pulsed power stage is designed to accelerate the projectile further to a velocity of 700 m/s.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1997
- Accession Number
- ADA322875
Entities
People
- E. Kathe
- E. Levi
- M. Cipollo
- P. M. Vottis
- Z. Zabar
Organizations
- United States Army Armament Research, Development and Engineering Center