Non-Eroding Hot Gas Components for Strategic Propulsion Systems Produced by Reduced Cost, Rapid Manufacturing Techniques

Period of Performance: 02/11/2014 - 08/11/2014

$80K

Phase 1 SBIR

Recipient Firm

Plasma Processes, LLC.
4914 Moores Mill Road Array
Huntsville, AL 35811
Principal Investigator

Abstract

Innovative solutions are sought to reduce cost and lead-time of hot gas valve components located in the post boost control system (PBCS) of the U.S. Navy s Trident II D-5 Fleet Ballistic Missile. Current PBCS components are based on Nb, Ta10W and TZM, with protective coatings. Although structurally sufficient and compatible with the oxidizing propellant, disadvantages include density, cost and lead-time. A concept promising to reduce weight, cost and lead-time is comprised of a carbon-based core and thin (i.e.