Rocket Propellant Testing Equipment
Project Requirements:
A new concept device to wire cut propellant samples from solid rocket motors. Possible pinch points used in previous designs were to be avoided as a possible ignition hazard.

Rocket  Propellant Testing Equipment
Solution:
A hydraulically actuated, remotely controlled device that uses a loose loop of wire to remove the sample in a two step procedure by cutting half way through from each side.
Ph# 530-620-7335