SBIR/STTR Research Award
COMPOSITE HEAT PIPE CONCEPTS USING PITCH GRAPHITE/METAL CPMPOSISTES
Award amount
$125,000Program and phase
SBIR · Phase IIAward year
1987Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- DWA ALUMINUM COMPOSITES
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- Not reported
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
FEASIBILITY WILL BE DEMONSTRATED FOR USE OF HIGH STIFFNESS HIGH THERMAL CONDUCTIVITY PITCH GRAPHIC REINFORCED-METAL COMPOSITES IN SIMPLE HEAT-PIPE CONCEPTS. THE VERY HIGHLY ANISOTROPIC THERMAL CONDUCTIVITY OF PITCH GRAPHITE, COMBINEDWITH EXCELLENT GR-METAL SPECIFIC MECHANICAL PROPERTIES SUGGESTS A "TAILORABLE" EFFICIENT MATERIAL FOR THERMAL-CONTROL SYSTEMS THAT BENEFIT FROM INTRINSIC STRUCTURAL INTEGRITY. SPACE STRUCTURE, SPACE CRAFT, AND MOST FLIGHT OR LAUNCHED SYSTEMS NECESSITATING THERMAL LOAD CONTROL CAN BENEFIT FROM THIS COMPOSITE THIS COMPOSITE CONCEPT. ALUMINUM MAXTRIX SYSTEMS WILL BE CONSIDERED FOR USE UP TO 500 DEGREES F, WHILE COPPER MATRICES COULD GO GEYOND 100 DEGREES F.
Technology keywords
Not reported