SBIR/STTR Research Award
HIGH TEMPERATURE COMPOSITE HOT HYDROGEN CONTROL VALVE DEVELOPMENT
Award amount
$49,834Program and phase
SBIR · Phase IAward year
1990Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- REFRACTORY COMPOSITES, INC.
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- Not reported
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
CERAMIC COMPOSITES PRESENTLY DEMONSTRATE GOOD MECHANICAL PROPERTIES AT TEMPERATURES BELOW 2100 DEG F WITHOUT DEGRADATION AND LOW THERMAL CONDUCTIVITY WITHOUT SACRIFICING THERMAL SHOCK TOLERANCE. THESE FACTORS COMBINED WITH LOW DENSITY AND LOW THERMAL EXPANSION CHARACTERISTICS MAKE THESE MATERIALS AN EXCELLENT CANDIDATE FOR A HIGH RESPONSE RATE VALVE MOVING PARTS WHILE LIMITING HOT VALVE THERMAL LOADS ON ELECTRICALLY POWERED ACTUATORS WITHOUT EXCESSIVE VOLUME OR WEIGHT PENALTIES. HOT HYDROGEN FLOW CONTROL AND SHUT-OFF VALVES WILL BE REQUIRED FOR SCRAMJET ENGINE CONTROL AND HYDROGEN COOLING CONTROL PURPOSES FOR MANNED HYPERSONIC VEHICLES. SUFFICIENT HOT HYDROGEN CORROSION DATA AND COMPOSITE FABRICATION TECHNOLOGIES HAVE BEEN DEVELOPED TO MAKE A QUANTUM LEAP IN HYDROGEN VALVE TECHNOLOGY FEASIBLE.
Technology keywords
Not reported