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Award ID | Description | Recipient | Total Value | Awarding Agency | Funding Agency | Set Aside | NAICS | PSC | Award Date | Start Date | End Date | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TPS QE B-25 FLIGHT COSTS | RAG WINGS & RADIALS AIRCRAFT LEASING LLC | $44,279 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 611512Flight Training | AR33 | Oct 21, 2019 | Oct 9, 2019 | Dec 7, 2019 | ||
| QE AW119KE ROTOR HEAD FLIGHT FLIGHT DEMO | AGUSTAWESTLAND PHILADELPHIA CORPORATION | $80,712 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 611512Flight Training | AR33 | Mar 21, 2019 | Apr 1, 2019 | Apr 12, 2019 | ||
| IGF::OT::IGF_TPS HU-16 QE FLIGHT COSTS | TALON AVIATION LLC | $48,847 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 611512Flight Training | AR33 | Feb 23, 2017 | Feb 16, 2017 | May 28, 2017 | ||
| IGF::OT::IGF | MISCELLANEOUS FOREIGN AWARDEES | $32,000 | STATE, DEPARTMENT OF | STATE, DEPARTMENT OF | — | 812930Parking Lots and Garages | AR33 | Jun 15, 2015 | Jun 15, 2015 | Jun 30, 2015 | ||
| IGF::OT::IGF 3DMAT PROJECT - SPECIALIZED RESIN PROCESING. NASA PROVIDES RAW MATERIALS. | M&P TECHNOLOGIES INC | $21,033 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR33 | Apr 25, 2013 | Apr 25, 2013 | Jul 31, 2013 | ||
| AIRBORNE LAUNCH ASSIST ACCESS (ALASA) RESEARCH AND DEVELOPMENT (R&D) - PHASE 1 | NORTHROP GRUMMAN SYSTEMS CORPORATION | $2,319,613 | DEFENSE CONTRACT MANAGEMENT AGENCY (DCMA) | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541712 | AR33 | Apr 19, 2012 | Apr 19, 2012 | Oct 19, 2013 | ||
| NASA IS DEVELOPING A SYSTEM TO FILTER CABIN AIR, CONCENTRATE A STREAM OF LOW PRESSURE HIGH PURITY OXYGEN, COMPRESS THE OXYGEN WITH AN ON BOARD COMPRESSOR, AND STORE THE OXYGEN IN THE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS CALLED HPGTS (HIGH PRESSURE GAS TANKS). THE OXYGEN PURITY REQUIREMENT FOR USE IN THE EMU (EVA MOBILITY UNIT, COMMONLY KNOWN AS THE SPACE SUIT ) IS GREATER THAN 99.5% PURITY. THE DELIVERY RATE TARGET IS 5 LBS O2 PER DAY. THE TARGET FOOTPRINT FOR THE OXYGEN SEPARATION SYSTEM IS THAT THE FLIGHT SYSTEM FIT WITHIN AN ENVELOPE MEASURING 20 X 20 X 24 INCHES. THE TARGET POWER CONSUMPTION IS 750 WATTS. COMMERCIAL OXYGEN SEPARATION SYSTEMS ARE TARGETED AT HOME MEDICAL OXYGEN APPLICATIONS. THE OXYGEN PURITY REQUIREMENT FOR HOME MEDICAL OXYGEN IS GREATER THAN 93% O2. HOME MEDICAL SYSTEMS ARE DESIGNED IN A WAY THAT PREVENT THE OXYGEN PURITY FROM BEING GREATER THAN 96%. DEVELOPING A FLIGHT OXYGEN SEPARATION SYSTEM REQUIRES A FUNDAMENTALLY NEW DESIGN. THIS FIRST STEP IN THE DESIGN PROCESS IS TO IDENTIFY, AND DEVELOP A SORBENT CAPABLE OF ACHIEVING HIGH OXYGEN PURITY. THE SECOND STEP IS TO INTEGRATE THIS SORBENT INTO AN OCM (OXYGEN CONCENTRATION MODULE), CAPABLE OF MEETING PRODUCTION RATE AND PURITY REQUIREMENTS. THE THIRD STEP IS DESIGNING AND MANUFACTURING THE BALANCE OF PLANT (VALVES, CONTROLLERS, COMPRESSORS) AND MANUFACTURING AND PACKAGING THE SYSTEM CAPABLE OF MEETING FLIGHT THERMAL, STRUCTURAL, AND ELECTRICAL REQUIREMENTS. TDA RESEARCH, IN THE COURSE OF SBIR CONTRACT NNX09CE30P, HAS DEMONSTRATED THE ABILITY TO SELECT AND MANUFACTURE OXYGEN SORBENT THAT MEETS UNIQUE FLIGHT SYSTEM REQUIREMENTS (NOT HOME MEDICAL REQUIREMENTS). TDA HAS DEMONSTRATED THE ABILITY TO DESIGN AND MANUFACTURE AIR SEPARATION SYSTEMS TO UNIQUE SPECIFICATIONS. TDA HAS DEMONSTRATED THE ABILITY TO DESIGN, DEVELOP, AND MANUFACTURE FULL SCALE SYSTEMS CAPABLE OF MEETING FLIGHT REQUIREMENTS. THE INTENT OF THIS CONTRACT IS TO LEVERAGE THE OXYGEN SEPARATION TECHNOLOGY DEVELOPED IN THE COURSE OF NNX09CE30P, AND DETERMINE IF THIS CAPABILITY CAN BE APPLIED DEVELOP A COMPACT, SPACE RATED, HIGH PURITY OCM. THE FIRST STEP TOWARDS DEVELOPING THIS CAPABILITY IS SELECTING, MANUFACTURING, AND CHARACTERIZING THE APPROPRIATE OXYGEN SEPARATION SORBENT. IN THE COURSE OF NNJ10HD25P, TDA RESEARCH SUCCESSFULLY SELECTED A SORBENT (A SILVER EXCHANGED LITHIUM BASED TYPE X SORBENT), MANUFACTURED THE SORBENT IN SMALL (50 CC/BATCH) BATCHES, AND CHARACTERIZED THE SORBENT PERFORMANCE (O2/AR SEPARATION COEFFICIENT IS 1.20 AT 20 DEGREES C, 1.8 ATM). | TDA RESEARCH, INC. | $62,400 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR33 | Jan 5, 2011 | Jan 5, 2011 | Mar 9, 2011 | ||
| LASER TRACKER RENTAL | HENRY SERVIN & SONS, INC. | $4,500 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 532490Other Commercial and Industrial Machinery and Equipment Rental and Leasing | AR33 | Nov 17, 2010 | Dec 1, 2010 | Dec 30, 2010 | ||
| NASA PRESENTLY PROVIDES THE HIGH PURITY, HIGH PRESSURE OXYGEN USED BY THE EVA MOBILITY UNIT (EMU, OR SPACESUIT) WITH SHUTTLE DERIVED OXYGEN. THE OXYGEN IS LAUNCHED ON THE SHUTTLE AS A CRYOGENIC FLUID, TRANSFERRED TO THE INTERNATIONAL SPACE STATION (ISS) AS A MODERATE PRESSURE GAS USING A TRANSFER HOSE, FURTHER COMPRESSED USING AN ONBOARD COMPRESSOR, AND STORED IN LARGE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. AFTER THE SHUTTLE RETIRES, ISS WILL CONTINUE TO CONDUCT EVAS AND NEED A NEW SUPPLY OF HIGH PRESSURE HIGH PURITY OXYGEN. THE ISS USES WATER ELECTROLYSIS TO PROVIDE LOW PRESSURE OXYGEN FOR METABOLIC CONSUMPTION. NASA IS DEVELOPING A SYSTEM TO FILTER CABIN AIR, CONCENTRATE A STREAM OF LOW PRESSURE HIGH PURITY OXYGEN, COMPRESS THE OXYGEN WITH AN ON BOARD COMPRESSOR, AND STORE THE OXYGEN IN THE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. THE OXYGEN PURITY REQUIREMENT FOR USE IN THE EMU IS GREATER THAN 99.5% PURITY. THE DELIVERY RATE TARGET IS 5 LBS O2 PER DAY. THE SEPARATION SYSTEM NEEDS TO OPERATE IN THE ISS ENVIRONMENT. ONE OF THE APPROACHES FOR OXYGEN CONCENTRATION USES A TWO BED, SINGLE STAGE, VACUUM PRESSURE SWING ADSORPTION (VPSA) SYSTEM. NASA HAS COLLECTED PERFORMANCE DATA FROM TWO DIFFERENT VPSA DEVICES. THE FIRST DEVICE IS A SUB SCALE PROTOTYPE UNIT, THAT MEETS O2 PURITY REQUIREMENTS, BUT PRODUCES LESS THAN 5 LBS PER DAY. THE SUBSCALE DEVICE USES A SORBENT DESCRIBED IN US PATENT 6,432,170. THE PATENT HOLDERS DO NOT HAVE ADDITIONAL SORBENT MATERIAL AVAILABLE FOR USE BY NASA. BECAUSE NASA NEEDS A RELATIVELY SMALL AMOUNT OF SORBENT (NOMINALLY 250 LBS FOR THE ENTIRE SYSTEM, INCLUDING RESERVE MATERIAL), THE PATENT HOLDERS CANNOT PRODUCE A COMMERCIALLY VIABLE BATCH OF SORBENT SPECIFICALLY FOR NASA. NASA S SECOND PROTOTYPE SYSTEM IS A FULL SCALE, TWO BED, SINGLE STAGE, VPSA SYSTEM CAPABLE OF PRODUCING MORE THAN 5 LBS OF OXYGEN PER DAY. BECAUSE OF SORBENT LIMITATIONS, THIS SYSTEM IS NOT CAPABLE OF MEETING THE 99.5% O2 PURITY REQUIREMENT. NASA SEEKS TO TEST THE PERFORMANCE OF CANDIDATE SORBENTS IN THE 5 LB PER DAY PROTOTYPE UNIT. ADDITIONALLY, NASA SEEKS TO ASSESS KEY SORBENT PERFORMANCE CHARACTERISTICS. NASA IS WILLING TO CONSIDER ANY SORBENTS THAT ARE CAPABLE OF PRODUCING AN OXYGEN STREAM WITH GREATER THAN 99.5% PURITY WHEN CONCENTRATING STANDARD AIR. ONE APPROACH WOULD BE TO USE THE MATERIAL SPECIFIED IN US PATENT 6,432,170, ASSIGNED TO AIR PRODUCTS AND CHEMICALS, INC. (CONTACT JEFF KNOPF @ [email protected]). NASA IS ALSO INTERESTED IN OTHER SORBENTS CAPABLE OF SEPARATING HIGH PURITY OXYGEN FROM AIR. IF TEST RESULTS ARE FAVORABLE, NASA MAY PURCHASE SORBENT FOR OXYGEN SEPARATION SYSTEMS. THE NOMINAL BATCH SIZE OF THIS ORDER IS 250 LBS (MAYBE MORE, MAYBE LESS, DEPENDING ON THE COST OF THE MATERIAL). NASA INTENDS TO AWARD (UP TO THREE) PURCHASE ORDER CONTRACTS. NASA WILL OBTAIN A RESEARCH REPORT AS A PRODUCT. THE TECHNICAL ACTIVITIES WILL REQUIRE THE CONTRACTOR TO DEVELOP AND CHARACTERIZE SORBENTS CAPABLE OF PRODUCING HIGH PURITY OXYGEN FROM AIR. | HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 336413Other Aircraft Parts and Auxiliary Equipment Manufacturing | AR33 | Aug 31, 2010 | Sep 1, 2010 | Jan 21, 2011 | ||
| SBIR PHASE III-OXYGEN SEPARATION SORBENT FEASIBILITY STUDY NASA IS DEVELOPING A SYSTEM TO FILTER CABIN AIR, CONCENTRATE A STREAM OF LOW PRESSURE HIGH PURITY OXYGEN, COMPRESS THE OXYGEN WITH AN ON BOARD COMPRESSOR, AND STORE THE OXYGEN IN THE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. THE OXYGEN PURITY REQUIREMENT FOR USE IN THE EMU(EVA MOBILITY UNIT, COMMONLY KNOWN AS THE SPACE SUIT ) IS GREATER THAN 99.5% PURITY. THE DELIVERY RATE TARGET IS 5 LBS O2 PER DAY. THE SEPARATION SYSTEM WILL OPERATE IN THE INTERNATIONAL SPACE STATION (ISS) ENVIRONMENT. ONE OF THE APPROACHES FOR OXYGEN CONCENTRATION USES A TWO BED, SINGLE STAGE, VACUUM PRESSURE SWING ADSORPTION (VPSA) SYSTEM. NASA HAS COLLECTED PERFORMANCE DATA FROM TWO DIFFERENT VPSA DEVICES. THE FIRST DEVICE IS A SUB SCALE PROTOTYPE UNIT, THAT MEETS O2 PURITY REQUIREMENTS, BUT PRODUCES LESS THAN 5 LBS PER DAY. THE SUBSCALE DEVICE USES A SORBENT DESCRIBED IN US PATENT 6,432,170. THE PATENT HOLDERS DO NOT HAVE ADDITIONAL SORBENT MATERIAL AVAILABLE FOR USE BY NASA. BECAUSE NASA NEEDS A RELATIVELY SMALL AMOUNT OF SORBENT (NOMINALLY 250 LBS FOR THE ENTIRE SYSTEM, INCLUDING RESERVE MATERIAL), THE PATENT HOLDERS CANNOT PRODUCE A COMMERCIALLY VIABLE BATCH OF SORBENT SPECIFICALLY FOR NASA. NASA S SECOND PROTOTYPE SYSTEM IS A FULL SCALE, TWO BED, SINGLE STAGE, VPSA SYSTEM CAPABLE OF PRODUCING MORE THAN 5 LBS OF OXYGEN PER DAY. BECAUSE OF SORBENT LIMITATIONS, THIS SYSTEM IS NOT CAPABLE OF MEETING THE 99.5% O2 PURITY REQUIREMENT. BACKGROUND NASA PRESENTLY PROVIDES THE HIGH PURITY, HIGH PRESSURE OXYGEN USED BY THE EVA MOBILITY UNIT (EMU, OR SPACESUIT) WITH SHUTTLE DERIVED OXYGEN. THE OXYGEN IS LAUNCHED ON THE SHUTTLE AS A CRYOGENIC FLUID, TRANSFERRED TO THE ISS AS A MODERATE PRESSURE GAS USING A TRANSFER HOSE, FURTHER COMPRESSED USING AN ONBOARD COMPRESSOR, AND STORED IN LARGE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. AFTER THE SPACE SHUTTLE RETIRES, ISS WILL CONTINUE TO CONDUCT EVAS AND NEED A NEW SUPPLY OF HIGH PRESSURE HIGH PURITY OXYGEN. THE ISS USES WATER ELECTROLYSIS TO PROVIDE LOW PRESSURE OXYGEN FOR METABOLIC CONSUMPTION. | TDA RESEARCH, INC. | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR33 | Aug 19, 2010 | Aug 20, 2010 | Sep 24, 2010 | ||
| GPS IIF-9 MISSION ORDER CLINS 0100-0101 | LOCKHEED MARTIN CORP | $51,153,741 | DEPT OF THE AIR FORCE | Department of the Air Force | — | 336414Guided Missile and Space Vehicle Manufacturing | AR33 | May 5, 2010 | May 5, 2010 | Sep 30, 2012 | ||
| END OF YEAR FY06 | UNITED LAUNCH SERVICES, LLC | $0 | DEPT OF THE AIR FORCE | Department of the Air Force | — | 336414Guided Missile and Space Vehicle Manufacturing | AR33 | Feb 22, 2010 | Feb 22, 2010 | Dec 31, 2010 | ||
| END OF YEAR FY09 PROCESSING | UNITED LAUNCH SERVICES, LLC | $1,380,770,000 | DEFENSE CONTRACT MANAGEMENT AGENCY (DCMA) | DEPT OF THE AIR FORCE | — | 336414Guided Missile and Space Vehicle Manufacturing | AR33 | Sep 30, 2009 | Sep 30, 2009 | Sep 16, 2011 | ||
| TECHNICAL GOALS AND OBJECTIVES THE OBJECTIVE OF THIS PROGRAM IS TO OBTAIN A SAFER LI-ION RECHARGEABLE CELL FOR ENERGY STORAGE THAT DOES NOT GO INTO FLAMES UNDER ABUSIVE CONDITIONS SUCH AS OVERCHARGE, OVERDISCHARGE, AND EXTERNAL SHORT CONDITIONS. DEMONSTRATE BY TESTING THE ABSENCE OF FIRE UNDER ABUSIVE CONDITIONS; COMPLETION OF 500 CYCLES TEST; MICROCALORIMETER TEST TO DEMONSTRATE CALENDAR LIFE. FROM TRL 3 TO TRL 4 ETDP IS PROVIDING FUNDS FOR TESTING AND IS EXPECTED TO PICK UP FUTURE OPTIMIZATION AND SCALE-UP WORK. VALUE TO MISSION DIRECTORATES THE COLLABORATIVE WORK WITH QUALLION IS IN LINE WITH FUTURE ESMD GOALS TO OBTAIN A SAFE, HIGH ENERGY DENSITY LITHIUM-ION RECHARGEABLE BATTERY FOR APPLICATIONS SUCH AS THE LUNAR LANDER, ROVER AS WELL AS THE ADVANCED EVA SUIT BATTERIES. NASA S RETURN ON INVESTMENT (ROI) WILL BE REALIZED OVER BOTH THE SHORT AND LONG TERM. FLEXIBILITY IN CAPACITY SCALING AND BREAKTHROUGH IN SAFETY, ALLOWS ITS USE IN A WIDE VARIETY OF APPLICATIONS REQUIRING POWER AS FOR CREWED VEHICLES, ROBOTIC SURFACE MOBILITY SYSTEMS, CREW EQUIPMENT, ETC FOR LUNAR MISSIONS. CUSTOMER-SUPPLIER AGREEMENTS (CSA) HAVE BEING WORKED BETWEEN THE EXPLORATION EVA OFFICE AND THE ESMD-ENERGY STORAGE BATTERY PROJECT AS WELL AS THE ESMD AND THE LUNAR ARCHITECTURE TEAM (LAT2) TO ALIGN TECHNOLOGY DEVELOPMENT EFFORTS WITH FUTURE EXPLORATION REQUIREMENTS. TECHNICAL OBJECTIVE AND TEAM OBJECTIVE: TO DESIGN A SAFE LI-ION RECHARGEABLE CELL THAT DOES NOT GO INTO FLAMES UNDER ABUSIVE CONDITIONS SUCH AS OVERCHARGE AND EXTERNAL SHORT AND PROVIDE THE FOLLOWING CHARACTERISTICS: >120WH/KG; 1C CHARGE AND DISCHARGE WITH 3C 100 MS PULSE; 1000 CYCLE CAPABILITY WITH 70% CAPACITY RETENTION AT EOL; RE<100 MOHMS; SHOCK AND VIBE TOLERANCE TEAM: QUALLION OPTIMIZE DESIGN TO PROVIDE A CELL WITH SELF-EXTINGUISHING PROPERTIES NASA-JSC CARRY OUT TESTS ON SAMPLE CELLS NASA-GRC CARRY OUT CALORIMETER TESTS ACHIEVEMENT | Mobile Power Solutions, Inc. | $21,436 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541380Testing Laboratories and Services | AR33 | Apr 17, 2009 | Apr 20, 2009 | Sep 15, 2009 | ||
| SBIR PHASE III CONTRACT ENTITLED, "REDUCED GRAVITY CRYO-TRACKER TESTING AND ANALYSIS" | SIERRA LOBO INC | $99,225 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR33 | Sep 29, 2008 | Sep 30, 2008 | Oct 22, 2009 | ||
| LI-ION CELL PTC DEVICE CHARACTERIZATION FRANK DOLJACK OF RAYCHEM HAS PUBLISHED (IEEE TRANSACTIONS ON COMPONENTS, HYBRIDS, AND MANUFACTURING TECHNOLOGY) 4, 732, 1981) A METHOD TO FULLY CHARACTERIZE THE STEADY STATE (EQUILIBRIUM) AND THE TRANSIENT (NON-EQUILIBRIUM) STATE OF THEIR PTC RESISTORS. THIS DATA WILL ENABLE MATHEMATICAL MODELS OF FULL LITHIUM ION CELL DESIGNS TO BE MORE ACCURATE IN PREDICTING CELL BEHAVIOR IN OVER-CURRENT CONDITIONS. THE EQUILIBRIUM AND DYNAMIC RESPONSE CHARACTERISTICS OF 2 CELL POSITIVE THERMAL COEFFICIENT (PTC) DEVICE DESIGNS INSIDE LITHIUM ION CELLS WILL BE CHARACTERIZED AS A FUNCTION OF TEMPERATURE. THIS INVOLVES DETERMINING THE ULTIMATE TRIP CURRENT OF EACH DEVICE AS A FUNCTION OF TEMPERATURE AND THE HEAT DISSIPATION RATE IN THE TRIPPED STATE. FIFTEEN (15) CELLS OF EACH DESIGN (PANASONIC CGR-18650C AND MOLI ICR-18650J) WILL BE PROVIDED BY NASA. THESE CELLS HAVE VIRGIN PTC DEVICES. MINIMUM AND MAXIMUM BASE RESISTANCES VERSUS TEMPERATURE THE MINIMUM VALUE SHALL BE OBTAINED BY SELECTING NEVER TRIPPED (VIRGIN) HEADER ONLY DEVICES AND MEASURING THE RESISTANCE TO 5% DURING A SLOW CONTINUOUS SWEEP OF TEMPERATURES BETWEEN 5 & 180 C WITH EMPHASIS IN THE 120 TO 140 C REGION. THE MAXIMUM VALUE SHALL BE OBTAINED BY THE SAME METHOD EXCEPT USING DEVICES THAT HAVE BEEN TRIPPED ONCE AND ALLOWED TO RECOVER FOR AT LEAST 24 HOURS PRIOR TO TEST. CURRENT VS VOLTAGE CHARACTERIZATION OF IN-CELL PTC DEVICES THIS TASK REQUIRES MEASURING THE VOLTAGE DROP ACROSS THE PTC DEVICE OF LITHIUM ION CELLS WHILE INSIDE AND OUTSIDE THE CELL. POWER DISSIPATION RATE THIS TASK CONNECTS THE CELL UNDER TEST IN SERIES WITH A POWER SUPPLY LIMITED TO 21 1V. A TEST REPORT SHALL BE PROVIDED WITH METHODS USED AND ALL TEST RESULTS WITHIN 2 MONTHS AFTER CONTRACT START DATE. THE TEST REPORT REQUIREMENTS ARE: PLOT OF MINIMUM AND MAXIMUM BASE RESISTANCE VS TEMPERATURE FOR EACH CELL DESIGN OR COMBINED ON THE SAME PLOT. PLOT OF CURRENT VS VOLTAGE CURVES AT EACH TEMPERATURE FOR A CELL DESIGN, SIMILAR TO FIG 8 OF DOLJACK S PAPER. PLOT OF THE POWER DISSIPATION RATE VS TEMPERATURE CURVES FOR BOTH CELL DESIGNS ON THE SAME PLOT. | SYMMETRY RESOURCES, INC | $22,840 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541380Testing Laboratories and Services | AR33 | Jun 11, 2008 | Jun 11, 2008 | Aug 19, 2008 | ||
| COTS-DEMONSTRATION OF COMMERICAL ORBITAL TRANSPORTATION SERVICES | ORBITAL SCIENCES LLC | $288,000,000 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | AR33 | Feb 19, 2008 | Feb 19, 2008 | Feb 19, 2013 | ||
| END OF YEAR FY07 PROCESSING | THE BOEING COMPANY | $6,552,468 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 336414Guided Missile and Space Vehicle Manufacturing | AR33 | Sep 30, 2007 | Sep 30, 2007 | Dec 31, 2010 | ||
| SAP PURCHASE REQUISITION: 4200200839 THERMAL MEASUREMENTS FOR CEV TPS AND ADP. THIS DATA WILL AFFECT THE DESIGN OF THE HEAT SHIELD CURRENTLY UNDERWAY. | THERMOPHYSICAL PROPERTIES RESEARCH LABORATORY, INC. | $5,535 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 927110Space Research and Technology | AR33 | May 23, 2007 | May 23, 2007 | Jun 21, 2007 | ||
| TAS::80 0124::TAS DESIGN, DEVELOPMENT, TEST&EVALUATION OF PROJECT ORION | LOCKHEED MARTIN CORP | $16,064,596,124 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541710 | AR33 | Aug 31, 2006 | Sep 6, 2006 | Sep 30, 2026 | ||
| PERFORMANCE OPTIMIZATION OF STORABLE BIPROPELLANT ENGINES TO FULLY EXPLOIT ADVANCED MATERIAL TECH | AEROJET ROCKETDYNE, INC. | $3,445,337 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 336415Guided Missile and Space Vehicle Propulsion Unit and Propulsion Unit Parts Manufacturing | AR33 | Aug 30, 2006 | Aug 30, 2006 | Dec 31, 2009 | ||
| COMPUTER MESH DEV | THOMPSON, DAVID | $20,000 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | — | AR33 | Aug 24, 2006 | Aug 23, 2006 | Feb 28, 2007 | ||
| DEMONSTRATION OF COMMERICAL ORBITAL TRANSPORTATION SERVICES (COTS) | SPACE EXPLORATION TECHNOLOGIES CORP. | $586,299,995 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | AR33 | Aug 18, 2006 | Aug 18, 2006 | Dec 31, 2012 | ||
| DEMONSTRATION OF COMMERICAL ORBITAL TRANSPORTATION SERVICES (COTS) | ROCKETPLANE LIMITED INCORPORATED | $406,800,000 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | — | AR33 | Aug 18, 2006 | Aug 18, 2006 | Apr 30, 2012 | ||
| CONDUCTIVE COATINGS FOR EVA VISORS | CLEVELAND STATE UNIVERSITY | $7,728 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | — | AR33 | Jun 2, 2006 | Jun 2, 2006 | Sep 30, 2006 |