Pm. Vottis et al., USE OF ELECTROMAGNETIC COIL LAUNCHER TO INCREASE MUZZLE VELOCITY OF CONVENTIONAL CANNONS, IEEE transactions on magnetics, 33(1), 1997, pp. 190-194
The paper deals with the design and operation of an experimental hybri
d cannon consisting of a 60 mm bore gas cannon using standard propella
nt and a traveling-wave induction accelerator. The projectile, consist
ing of an aluminum cylinder weighing 120 grams, is initially brought u
p to a speed of 600 m/s in the gas cannon. The pulsed-power stage is d
esigned to accelerate the projectile further to a velocity of 700m/s.