You are here
THERMACORE, INC.
UEI: HUT3XNPLRL77
# of Employees: 185
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
-
SORPTION RESERVOIRS FOR THERMIONIC CONVERTERS
Amount: $74,528.00N/A
SBIRPhase I1989Department of Defense Missile Defense Agency -
HEAT PIPE COOLING OF FARADAY SHIELDS
Amount: $49,971.00N/A
SBIRPhase I1989Department of Energy -
SPACECRAFT HEAT REJECTION METHODS
Amount: $499,000.00MANY NEAR-FUTURE MILITARY SATELLITES WILL HAVE POWER REQUIREMENTS OF FIVE TO TEN KILOWATTS. THIS REQUIREMENT IS EXPECTED TO GROW TO 100 KW OR MORE DURING THE NEXT TWENTY YEARS. THE MUCH HIGHER HEAT LO ...
SBIRPhase II1988Department of Defense Missile Defense Agency -
HIGH TEMPERATURE CAPILLARY PUMPED LOOP HEAT PIPE
Amount: $498,000.00DESIGNS FOR SPACE BASED STRUCTURES ARE BECOMING INCREASINGLY LARGER AND MORE COMPLEX. AS THESE STRUCTURES GROW, THEIR LEVEL OF POWER CONSUMPTION IS ALSO INCREASING. TO SATISFY THIS DEMAND FOR POWER, E ...
SBIRPhase II1988Department of Defense Missile Defense Agency -
FLEXIBLE HEAT PIPE COLD PLATE
Amount: $500,000.00FEEDBACK POSITIONING AND CONTROL OF ONE FLIGHT CONTROL HYDRAULIC ACTUATOR REQUIRES DOZENS OF WIRES BETWEEN THE ACTUATOR AND FLIGHT CONTROL COMPUTER. IT IS DESIRABLE TO REDUCE THIS WIRE COUNT BY INCORP ...
SBIRPhase II1988Department of Defense Navy -
ADVANCED HEAT PIPES FOR AVLIS COLLECTOR PLATE COOLING
Amount: $494,000.00THE USE OF HEAT PIPES CAN GREATLY SIMPLIFY THE DIFFICULT PROBLEM OF COOLING THE PRODUCT COLLECTOR PLATES IN THE ATOMIC VAPOR LASER ISOTOPE SEPARATION (AVLIS) TECHNIQUE. BECAUSE OF VERY TIGHT SPACE REQ ...
SBIRPhase II1988Department of Energy -
CARBON FIBER REINFORCED CERAMIC WING LEADING EDGE HEAT PIPES
Amount: $59,036.00CURRENT HYPERSONIC AIRCRAFT DESIGNS REQUIRE COOLING ON THEIR LEADING EDGE SURFACES. HEAT PIPES HAVE THE POTENTIAL OF PROVIDING A LOWWEIGHT METHOD OF COOLING THESE SURFACES. HOWEVER, CURRENT HEAT PIPE ...
SBIRPhase I1988Department of Defense Air Force -
PASSIVE VARIABLE THERMAL RESISTANCE TECHNIQUES
Amount: $500,000.00SOME MISSILE INERTIAL GUIDANCE SYSTEMS USE THE MISSILE STRUCTURE AS A HEAT SINK. THE HEAT SINK TEMPERATURE CHANGES DURING THE ELAPSED TIME BETWEEN LAUNCH AND WHEN THE MISSILE BECOMES BALLISTIC. THIS C ...
SBIRPhase II1987Department of Defense Navy -
ADVANCED HEAT PIPE BODY MOUNTED RADIATORS
Amount: $49,907.00AS THE NUMBER OF ACTIVITIES PLANNED FOR THE SPACE STATION, AND THEIR ASSOCIATED ENERGY REQUIREMENTS CONTINUE TO GROW, CONCERN OVER THERMAL MANAGEMENT IS INCREASING. ONE AREA OF CURRENT DEVELOPMENT IS ...
SBIRPhase I1987National Aeronautics and Space Administration -
TITANIUM/WATER CAPILLARY PUMPED LOOP FOR MANNED ENVIRONMENTS
Amount: $49,907.00FUTURE SPACE SYSTEMS WILL UNDOUBTEDLY UTILIZE TWO-PHASE HEAT TRANSPORT DEVICES TO MANAGE THEIR COMPLEX THERMAL SYSTEMS. MANY CONCEPTS HAVE BEEN PROPOSED FOR A TWO-PHASE THERMAL BUS SUCH AS HEAT PIPES, ...
SBIRPhase I1987National Aeronautics and Space Administration