Federal Contractor Profile
Advanced Cooling Technologies INC
$66M obligated·144 awards·4 agencies·15 NAICS
Federal Contracts
Showing contracts 151–176 of 176 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Jan 6, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CJ55P | 541712 | IGF::OT::IGF ADVANCED COOLING TECHNOLOGIES, INC. (ACT) HAS DEVELOPED A NOVEL KIND OF HYBRID HEAT PIPES TO SOLVE THE HIGH HEAT FLUX LIMITATION FOR FUTURE HIGHLY INTEGRATED SPACECRAFT INSTRUMENTS AND ELECTRONICS. THESE HYBRID HEAT PIPES WILL BE CAPABLE OF OPERATING AT THE HIGHER HEAT FLUX REQUIREMENTS (50W/CM2) EXPECTED IN NASA'S FUTURE SPACECRAFT AND INSTRUMENTS SUCH AS THE NEXT GENERATION OF ROVERS AND LANDERS AND WITH THE POSSIBILITY OF BEING USED IN MANNED SPACECRAFT'S AND EXTRATERRESTRIAL HABITATS. THESE HYBRID HEAT PIPES CAN ALSO (I) OPERATE AGAINST GRAVITY ON PLANETARY SURFACES, (II) OPERATE IN SPACE CARRYING POWER OVER LONG DISTANCES AND (III) ACT AS A THERMOSYPHON ON THE PLANETARY SURFACE FOR LUNAR AND MARTIAN LANDERS AND ROVERS. IN MANY CASES, THEY CAN REPLACE LOOP HEAT PIPES (LHPS) ON LANDERS AND ROVERS. LHPS ARE MORE COMPLICATED TO OPERATE, AND ARE TWO ORDERS OF MAGNITUDE MORE EXPENSIVE. IN PHASE 1 ACT DESIGNED, FABRICATED, TESTED AND SUCCESSFULLY DEMONSTRATED THIS CONCEPT WITH THE FABRICATION OF 4 CONSTANT CONDUCTANCE HEAT PIPES. THIS PHASE 3 REQUIRES ACT TO MANUFACTURE A RADIATOR CAPABLE OF SHUTTING OFF THE RADIATIVE HEAT REJECTION WHILE WORK UNDER AN ADVERSE GRAVITATIONAL ENVIRONMENT WITH THE USE OF THIS NOVEL TYPE OF HYBRID HEAT PIPES. THIS HARDWARE WILL BE INTEGRATED WITH THE GROUND TEST ADVANCED PASSIVE THERMAL EXPERIMENT (APTX) WHICH IS PART OF THE NASA JOHNSON SPACE CENTERS (JSC) DISCIPLINES TECHNOLOGY DEVELOPMENT EFFORT. THIS EFFORT INTENDS TO FILL SOME OF THE CURRENT TECHNICAL GAPS NEEDED TO BE ADDRESSED FOR FUTURE HUMAN EXPLORATION ARCHITECTURES. | $15K |
| Dec 16, 2016 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV16C0016 | 541712 | IGF::OT::IGF PHASE II SBIR FOR A NON-CATALYTIC JP-8 REFORMER. | $500K |
| Dec 6, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001417P1004 | 541712 | SBIRSOL2016.2 IGF::CT::IGF | $80K |
| Dec 6, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001417P2017 | 541712 | SBIRSOL2016.2 IGF::CT::IGF | $80K |
| Oct 20, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833517C0024 | 541712 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $80K |
| Sep 26, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0114 | 541712 | IGF::OT::IGF RESEARCH AND DEVELOPMENT | $375K |
| Sep 9, 2016 | Department of DefenseFA2487 AFTC PZZD (EGLIN) | FA248715C0326 | 541712 | IGF::OT::IGF SBIR PHASE 2 - HIGH ACCURACY TURNKEY | $375K |
| Sep 7, 2016 | Department of DefenseFA9453 AFRL RVK | FA945316M0446 | 541712 | IGF::OT::IGF HIGH TEMPERATURE LIGHTWEIGHT HEAT PIPES FOR SOLID-STATE POWER AMPLIFIER THERMAL MANAGEMENT | $150K |
| Aug 15, 2016 | Department of DefenseNAVAL AIR WARFARE CENTER | N6893616P0732 | 334511 | CENTER SHAFT BASE&TABLE WING ASSEMBLIE | $68K |
| Aug 8, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833515C0032 | 541712 | STTR PHASE II RESEARCH AND DEVELOPMENT | $250K |
| Jul 6, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M2695 | 541712 | IGF::OT::IGF ADVANCED COOLING SBIR I | $150K |
| Jul 6, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016M2692 | 541712 | IGF::OT::IGF SBIR I APPARATUS FOR EVALUATING CHEMICAL COMPOSITION OF TOOLS | $150K |
| Jun 30, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CJ55P | 541712 | IGF::OT::IGF ADVANCED COOLING TECHNOLOGIES, INC. (ACT) HAS DEVELOPED A NOVEL KIND OF HYBRID HEAT PIPES TO SOLVE THE HIGH HEAT FLUX LIMITATION FOR FUTURE HIGHLY INTEGRATED SPACECRAFT INSTRUMENTS AND ELECTRONICS. THESE HYBRID HEAT PIPES WILL BE CAPABLE OF OPERATING AT THE HIGHER HEAT FLUX REQUIREMENTS (50W/CM2) EXPECTED IN NASA'S FUTURE SPACECRAFT AND INSTRUMENTS SUCH AS THE NEXT GENERATION OF ROVERS AND LANDERS AND WITH THE POSSIBILITY OF BEING USED IN MANNED SPACECRAFT'S AND EXTRATERRESTRIAL HABITATS. THESE HYBRID HEAT PIPES CAN ALSO (I) OPERATE AGAINST GRAVITY ON PLANETARY SURFACES, (II) OPERATE IN SPACE CARRYING POWER OVER LONG DISTANCES AND (III) ACT AS A THERMOSYPHON ON THE PLANETARY SURFACE FOR LUNAR AND MARTIAN LANDERS AND ROVERS. IN MANY CASES, THEY CAN REPLACE LOOP HEAT PIPES (LHPS) ON LANDERS AND ROVERS. LHPS ARE MORE COMPLICATED TO OPERATE, AND ARE TWO ORDERS OF MAGNITUDE MORE EXPENSIVE. IN PHASE 1 ACT DESIGNED, FABRICATED, TESTED AND SUCCESSFULLY DEMONSTRATED THIS CONCEPT WITH THE FABRICATION OF 4 CONSTANT CONDUCTANCE HEAT PIPES. THIS PHASE 3 REQUIRES ACT TO MANUFACTURE A RADIATOR CAPABLE OF SHUTTING OFF THE RADIATIVE HEAT REJECTION WHILE WORK UNDER AN ADVERSE GRAVITATIONAL ENVIRONMENT WITH THE USE OF THIS NOVEL TYPE OF HYBRID HEAT PIPES. THIS HARDWARE WILL BE INTEGRATED WITH THE GROUND TEST ADVANCED PASSIVE THERMAL EXPERIMENT (APTX) WHICH IS PART OF THE NASA JOHNSON SPACE CENTERS (JSC) DISCIPLINES TECHNOLOGY DEVELOPMENT EFFORT. THIS EFFORT INTENDS TO FILL SOME OF THE CURRENT TECHNICAL GAPS NEEDED TO BE ADDRESSED FOR FUTURE HUMAN EXPLORATION ARCHITECTURES. | $63K |
| Jun 30, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ16HK20P | 541712 | VHC COPPER BODY AND HIK PLATE. | $45K |
| Jun 15, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0301 | 541712 | PROGRESS REPORT R&D IGF::OT::IGF | $80K |
| Jun 3, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CM46P | 541712 | IGF::OT::IGF ADVANCED COOLING TECHNOLOGIES, INC. (ACT) PROPOSES TO DEVELOP A LOW-COST LOOP HEAT PIPE (LHP) EVAPORATOR USING A TECHNIQUE KNOWN AS DIRECT METAL LASER SINTERING (DMLS), OTHERWISE KNOWN AS 3D PRINTING, TO PRODUCE LOW-COST LHPS TO BE USED IN CUBESAT AND SMALLSAT APPLICATIONS. THE WICK STRUCTURE IN AN LHP ASSUMES THE ROLE OF A PUMP IN A STANDARD LOOP, PUMPING LIQUID FROM THE LOWER PRESSURE CONDENSER TO THE HIGHER PRESSURE EVAPORATOR BY CAPILLARY FORCES. THE OVERALL THERMAL PERFORMANCE OF THE SYSTEM IS THEREFORE HIGHLY DEPENDENT ON THE IN-SITU CHARACTERISTICS OF THE WICK STRUCTURE. CURRENT LHP WICK MANUFACTURING AND INSTALLATION PROCESSES ARE CUMBERSOME, LABOR INTENSIVE, AND SUFFER FROM A LOW YIELD RATE. SPECIFICALLY, THE PRIMARY WICK?S HYDRODYNAMIC CHARACTERISTICS AND SEALING INTEGRITY TO THE ENVELOPE ARE CRITICAL TO HEAT TRANSPORT, START-UP, SHUT DOWN AND OVERALL RELIABILITY. IT IS ESTIMATED THAT THE COST TO PRODUCE AN LHP EVAPORATOR, INCLUDING THE ATTACHMENT OF THE BAYONET, SECONDARY WICK AND COMPENSATION CHAMBER, ACCOUNTS FOR APPROXIMATELY 75% OF THE TOTAL SYSTEM?S MANUFACTURING COST. BY 3D PRINTING AN EVAPORATOR ENVELOPE WITH AN INTEGRAL POROUS PRIMARY WICK STRUCTURE, THE OVERALL COMPLEXITY AND COST OF THE DESIGN CAN BE SIGNIFICANTLY REDUCED. | $125K |
| Jun 3, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CG54P | 541712 | IGF::OT::IGF SPECIFIC MISSION REQUIREMENTS CAN OFTEN REQUIRECALL FOR SOME DEGREE OF FLEXIBILITY SUCH AS MINIMIZING MECHANICAL LOADS INDUCED INTO PAYLOADS CONTAINING HIGHLY SENSITIVE POSITIONAL SENSORS OR ALLOWING CONTAINMENT OF RADIATOR PANELS WITHIN SPACECRAFT FAIRING UNTIL DEPLOYMENT INTO FULLY OPERATIONAL POSITIONS. FLEXIBLE THERMAL STRAPS AND LOOP HEAT PIPES (LHP) ARE TYPICALLY USED FOR THIS FLEXIBLE THERMAL LINK. THERMAL STRAPS ARE A LOWER TECHNOLOGY SOLUTION FOR LOWER HEAT TRANSPORT APPLICATIONS (<10 WATT) THAT NEED SMALL MECHANICAL DISPLACEMENT. LHPS CAN TRANSPORT KILOWATTS OF HEAT OVER LONG DISTANCES AND HAVE TRANSPORT LINES AND CONDENSER TUBES THAT ARE FLEXIBLE, BENDABLE, AND EASILY ROUTED THROUGH COMPLEX PATHS. DRAWBACKS OF LHPS INCLUDE BEING SIGNIFICANTLY MORE EXPENSIVE TO FABRICATE AND QUALIFY. FLEXIBLE CONSTANT CONDUCTANCE HEAT PIPES (CCHPS) CAN FILL THE GAP BETWEEN FLEXIBLE THERMAL STRAPS AND LOOP HEAT PIPES. THE SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PROGRAM PROPOSED BY ADVANCED COOLING TECHNOLOGIES, INC. (ACT) WILL DESIGN, FABRICATE, AND DEMONSTRATE A CRYOGENIC FLEXIBLE CCHP FOR A PASSIVE THERMAL MANAGEMENT DEVICE. | $125K |
| May 19, 2016 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ16HD49P | 333999 | ONE HIGH THERMAL CONDUCTIVITY (HIK) RADIATOR AND ONE HIK HEAT SPREADER PLATE | $29K |
| Apr 26, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0173 | 541712 | SBIR PI R&D. IGF::OT::IGF | $80K |
| Apr 22, 2016 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001414C0118 | 541712 | LONG RANGE BROAD AGENCY ANNOUNCEMENT (BAA) FOR NAVY AND MARINE CORPS SCIENCE AND TECHNOLOGY | $396K |
| Apr 21, 2016 | Department of DefenseNAVAL AIR WARFARE CENTER | N6893616P0265 | 334511 | NAWCWD CENTER SHAFT BASE AND TABLE | $4K |
| Feb 18, 2016 | Department of DefenseNAVAL AIR WARFARE CENTER | N6893616P0265 | 334511 | NAWCWD CENTER SHAFT BASE AND TABLE | $125K |
| Feb 11, 2016 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833516C0114 | 541712 | IGF::OT::IGF RESEARCH AND DEVELOPMENT | $375K |
| Dec 30, 2015 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV16C0016 | 541712 | IGF::OT::IGF PHASE II SBIR FOR A NON-CATALYTIC JP-8 REFORMER. | $500K |
| Dec 22, 2015 | Department of CommerceDEPT OF COMM/NAT INST STAND AND TECHNOL | DOCSB134116SU0070 | 332410 | IGF::OT::IGF-OTHER-PURCHASE ORDER FOR SODIUM ISOTHERMAL FURNACE LINERS | $120K |
| Oct 29, 2015 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001416P2005 | 541712 | IGF::CT::IGF ACTIVE THERMAL CONTROL SYSTEM OPTIMIZATION | $80K |
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