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Award ID | Description | Recipient | Total Value | Awarding Agency | Funding Agency | Set Aside | NAICS | PSC | Award Date | Start Date | End Date | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| AIR CHARTER FOR MEDICAL RE-DESIGNATION TO BHU | INFLIGHT MEDICAL SERVICES INTERNATIONAL, INC. | $15,723 | FEDERAL PRISON SYSTEM / BUREAU OF PRISONS | FEDERAL PRISON SYSTEM / BUREAU OF PRISONS | — | 621910Ambulance Services | AR34 | Feb 10, 2020 | Feb 10, 2020 | Mar 4, 2020 | ||
| IGF::OT::IGF DX-A2 FOUNTAINHEAD PR# 82-2003-17 | KINETIC RESEARCH CORPORATION | $6,000 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 541712 | AR34 | Dec 22, 2016 | Dec 22, 2016 | Jan 9, 2017 | ||
| IGF::OT::IGF HRL LABORATORIES, LLC, PROPOSES A 12 MONTH EFFORT TO DEVELOP AN ULTRA-LIGHTWEIGHT CORE MATERIAL THAT HAS HALF OR LESS THE DENSITY OF STATE-OF-THE-ART HONEYCOMB CORES, WHILE EXCEEDING THEIR MECHANICAL PROPERTIES. BY COMBINING OUR TEAM'S UNIQUE CAPABILITY TO MANUFACTURE ULTRALIGHT MICRO-TRUSS MATERIALS WITH OUR ABILITY TO DESIGN AND OPTIMIZE CELLULAR ARCHITECTURES, WE WILL ACHIEVE GROUNDBREAKING 40% MASS REDUCTION FOR SANDWICH STRUCTURES FOR FUTURE AEROSPACE VEHICLES. OUR APPROACH COMBINES MECHANICALLY EFFICIENT, ARCHITECTED MICRO-TRUSS TEMPLATES WITH HIGH-STRENGTH, NANOCRYSTALLINE METAL COATINGS. BOTH MANUFACTURING STEPS INVOLVED, HRL'S POLYMER MICRO-TRUSS FABRICATION AND ELECTROPLATING OF NANOCRYSTALLINE COATINGS, ARE INHERENTLY SCALABLE AND COST-EFFECTIVE, ENSURING THAT SCALE-UP TO LARGE STRUCTURES CAN BE ACHIEVED, WHILE MEETING NASA'S CHALLENGING COST TARGET. WE HAVE ALREADY FABRICATED 12X12X0.5 ULTRALIGHT MICRO-TRUSS CORES WITH A DENSITY OF 2 LB/FT3 AND SUPERIOR PROPERTIES TO SOA HONEYCOMB AS WELL AS CURVED MICRO-TRUSS SANDWICH PANELS FOR ONGOING DEVELOPMENT EFFORTS. UNDER THE PROPOSED EFFORT, WE WILL MATURE AND SCALE-UP NANOCRYSTALLINE METALLIC MICRO-TRUSS CORES FOR THE NEXT-GENERATION OF NASA'S ULTRA-LIGHTWEIGHT SANDWICH PANELS. | HRL LABORATORIES, LLC | $540,810 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 15, 2015 | Sep 15, 2015 | Oct 14, 2016 | ||
| IGF::OT::IGF REPLACE THE EXISTING HONEYCOMB-COMPOSITE SANDWICH STRUCTURES IN AEROSPACE VEHICLES AND STRUCTURES | DYNETICS, INC. | $549,928 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 15, 2015 | Sep 15, 2015 | Mar 7, 2018 | ||
| IGF::OT::IGF WBS 1.0 ULTRA LIGHTWEIGHT CORE DESIGN GENERATION. THE ATK TEAM WILL, ON A BEST EFFORTS BASIS, GENERATE AN ENGINEERED COMPOSITE CORE DESIGN THAT HAS A JUSTIFIABLE EXPECTATION OF MEETING THE TARGET CAPABILITIES LISTED IN THE NRA. THE BASIS FOR THE EXPECTATION WILL BE ROOTED IN ENGINEERING ANALYSES THAT APPLY FIRST PRINCIPLES OF ENGINEERING MECHANICS AND AVAILABLE MATERIALS INFORMATION TO EVALUATE CORE DESIGNS. THESE ANALYSES, INFORMATION, AND RELATED CALCULATIONS SHALL BE DOCUMENTED AND DELIVERED TO NASA. ANY SPREADSHEETS, COMPUTATIONAL TOOLS (SOURCE CODE), COMPUTER PROGRAMS (SOURCE CODE), CAD MODELS, AND FINITE ELEMENT MODELS DEVELOPED IN WBS 1.0, WITH ANY ATK PROPRIETARY PREEXISTING BACKGROUND INFORMATION, DATA, PROCESSES AND PROCEDURES EITHER REMOVED OR IDENTIFIED, SHALL BE DELIVERED TO NASA IN ELECTRONIC FORMAT SUFFICIENT FOR NASA TO PERFORM SIMILAR CALCULATIONS AND ANALYSES. A FINAL CORE DEFINITION THAT INCLUDES MATERIAL SELECTION, CORE CELL GEOMETRY, AND THE COMPOSITE LAMINATE DEFINITION WILL BE DOCUMENTED IN A TECHNICAL DRAWING. WBS 2.0 ULTRA LIGHTWEIGHT CORE PRODUCTION DEMONSTRATION. ATK WILL, ON A BEST EFFORTS BASIS, PROCURE ALL MATERIALS, TOOLING, AND LABOR REQUIRED TO FABRICATE THE CORE AS DOCUMENTED ON THE TECHNICAL DRAWINGS DEVELOPED IN WBS 1.0. SUFFICIENT CORE PIECES WILL BE PRODUCED TO SUPPORT TESTING BY ATK AND TO SUPPLY THE REQUIRED DELIVERABLE SEGMENTS TO NASA. THE DELIVERED ELECTRONIC DATA SHALL INCLUDE NOT ONLY THE POINT-WISE PERFORMANCE METRIC VALUES, BUT ALSO ALL ASSOCIATED DATA (E.G., CURVES) USED TO DETERMINE THE PERFORMANCE METRIC VALUES. WBS 3.0 PROCESS EVALUATIONS. ATK SHALL DEMONSTRATE THE ABILITY TO JOIN CORE SEGMENTS INTO EFFECTIVELY LARGER SEGMENTS AT EITHER AMBIENT CONDITIONS OR IN OVEN CURE ENVIRONMENTS. ATK SHALL DEMONSTRATE THE ABILITY TO ASSEMBLE AND CONSOLIDATE FACESHEETS TO THE CORE SEGMENTS IN BOTH FLAT AND CURVED PANEL CONFIGURATIONS USING CONVENTIONAL HONEYCOMB PANEL CONSOLIDATION TECHNIQUES. WBS 4.0 ULTRA LIGHTWEIGHT CORE PERFORMANCE EVALUATION. ATK SHALL, ON A BEST EFFORTS BASIS, GENERATE TEST DATA ON THE PRODUCED FLAT SANDWICH PANEL SEGMENT(S). THE TEST DATA SHALL BE SUFFICIENT TO COMPARE AND CONTRAST AGAINST THE TARGET PERFORMANCE METRICS IN THE NRA SOLICITATION. THE TEST DATA SHALL BE COMPARED AGAINST THE EXPECTED PERFORMANCE CAPABILITY DEVELOPED IN WBS 1.0, AND RECOMMENDATIONS FOR IMPROVING/OPTIMIZING PERFORMANCE SHALL BE COMPOSED. THE TEST DATA SHALL BE DOCUMENTED IN A REPORT, AS WELL AS STANDARD ELECTRONIC FORMAT, AND DELIVERED TO NASA. WBS 5.0 ULTRA LIGHTWEIGHT CORE COST PROJECTIONS. ATK SHALL, ON A BEST EFFORTS BASIS, DEVELOP A PLAN THAT LEADS TO PRICING REDUCTION OF THE ULTRA LIGHTWEIGHT CORE. WBS 6.0 DELIVERABLES. ATK SHALL, ON A BEST EFFORTS BASIS, DELIVER 4 EA. FLAT PANEL SEGMENTS AND 4 EA. PANEL SEGMENTS FOR CURVED APPLICATIONS TO NASA. ATK SHALL DELIVER QUARTERLY REPORTS AS REQUIRED. ATK SHALL DELIVER A FINAL ORAL REPORT AND A FINAL WRITTEN REPORT IN ACCORDANCE WITH THE NRA SOLICITATION. THE QUARTERLY AND FINAL REPORTS SHALL INCLUDE DETAILED DOCUMENTATION OF ALL METHODS AND CALCULATIONS USED TO ARRIVE AT THE COMPOSITE CORE DESIGN DEVELOPED IN WBS 1.0. ALL TEST DATA (KEY PERFORMANCE PARAMETERS AND ALL ASSOCIATED DATA TO DETERMINE THESE PERFORMANCE PARAMETERS) GENERATED IN WBS 4.0 SHALL BE DELIVERED TO NASA IN ELECTRONIC FORMAT. ANY DATA, SPREADSHEETS, COMPUTATIONAL TOOLS (SOURCE CODE), COMPUTER PROGRAMS (SOURCE CODE), CAD MODELS, AND FINITE ELEMENT MODELS DEVELOPED IN WBS 1.0, WITH ANY ATK PROPRIETARY PREEXISTING BACKGROUND INFORMATION, DATA, PROCESSES AND PROCEDURES EITHER REMOVED OR IDENTIFIED, SHALL BE DELIVERED TO NASA IN ELECTRONIC FORMAT SUFFICIENT FOR NASA TO PERFORM SIMILAR CALCULATIONS AND ANALYSES. ATK SHALL DEVELOP AND DELIVER A PROPOSAL FOR PHASE II. WBS 7.0 MANAGEMENT. ATK SHALL, ON A BEST EFFORTS BASIS, PROVIDE THE PROJECT MANAGEMENT AND OVERSIGHT NECESSARY TO EXECUTE THE TECHNICAL PLAN OUTLINED IN THIS PROPOSAL. | ATK SPACE SYSTEMS INC. | $407,044 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 15, 2015 | Sep 15, 2015 | Oct 15, 2016 | ||
| IGF::OT::IGF 1.1 BACKGROUND THE NEXT ION PROPULSION TECHNOLOGY HAS BEEN IN DEVELOPMENT BY THE NASA IN-SPACE PROPULSION TECHNOLOGY PROJECT, WITHIN THE SCIENCE MISSION DIRECTORATE (SMD), FOR USE IN A WIDE ARRAY OF ROBOTIC SCIENCE MISSIONS. A NEXT ION PROPULSION SYSTEM TYPICALLY CONSISTS OF GRIDDED ION THRUSTERS, POWER PROCESSING UNITS (PPUS), THRUSTER GIMBALS, A XENON PROPELLANT FEED SYSTEM, AND A CONTROL INTERFACE FUNCTIONALITY CAPTURED EITHER IN A DEDICATED UNIT OR DISTRIBUTED BETWEEN THE ION PROPULSION SYSTEM AND THE SPACECRAFT. NEXT IS APPLICABLE TO A BROAD ARRAY OF PLANETARY SCIENCE MISSIONS, INCLUDING DISCOVERY, NEW FRONTIERS AND FLAGSHIP MISSIONS AND ALSO HAS APPLICATION TO MULTIPLE CONCEPTUAL ASTROPHYSICS SCIENCE MISSIONS. 1.2 BASIS FOR PROCUREMENT THE NASA SMD PLANETARY SCIENCE DIVISION IS OFFERING NEXT FLIGHT HARDWARE, SPECIFICALLY TWO THRUSTERS AND TWO PPUS, AS GOVERNMENT-FURNISHED EQUIPMENT (GFE) FOR THE NEXT DISCOVERY MISSION ANNOUNCEMENT OF OPPORTUNITY (AO). THE DISCOVERY AO IS TARGETED FOR RELEASE IN OCTOBER 2014. REFER TO NASA SOLICITATION NUMBER NNH14ZDA009J FOR FURTHER INFORMATION REGARDING THE DISCOVERY AO AND TARGET SCHEDULES. NASA DESIRES FOR THE NEXT SYSTEM TO BE AVAILABLE TO FUTURE USERS AS A COMMERCIAL PRODUCT. NASA ENCOURAGES AND WILL CONSIDER MODIFICATIONS OR ALTERNATIVES TO THE EXISTING DESIGN, PARTICULARLY THE PPU DESIGN, TO FACILITATE MORE CONSISTENT USE IN NON-NASA APPLICATIONS. THEREFORE, THE FRAMEWORK FOR THIS PROCUREMENT AND THE FOLLOWING STATEMENT OF WORK IS FOR COST-SHARED DEVELOPMENT WHICH RESULTS IN PRODUCT USE FOR BOTH NASA AND NON-NASA MISSIONS. THE NASA PROJECT TO PROVIDE THIS GFE HARDWARE IS REFERRED TO AS THE NEXT-C PROJECT THROUGHOUT THIS DOCUMENT. | AEROJET ROCKETDYNE, INC. | $44,984,296 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Apr 2, 2015 | Mar 31, 2015 | Oct 9, 2020 | ||
| IGF::OT::IGF THE PURPOSE OF THIS PURCHASE IS FOR THE UPDATE AND RENEWAL OF CADRA SOFTWARE. | AEROSPACECOMPUTING, INC. | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541512Computer Systems Design Services | AR34 | Sep 26, 2013 | Sep 26, 2013 | Sep 30, 2014 | ||
| IGF::OT::IGF "OTHER FUNCTIONS" WIND TUNNEL TESTING SERVICES IN THE BOEING ST. LOUIS, POLYSONIC WIND TUNNEL (PSWT) FOR THE SPACE LAUNCH SYSTEMS (SLS) PROGRAM | THE BOEING COMPANY | $793,000 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 488190Other Support Activities for Air Transportation | AR34 | Aug 16, 2012 | Aug 16, 2012 | Nov 30, 2012 | ||
| SPACECRAFT TRAINING | KINETIC RESEARCH CORPORATION | $0 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 541330Engineering Services | AR34 | Jul 31, 2012 | Jul 31, 2012 | Aug 31, 2012 | ||
| THIS REQUIREMENT IS FOR THE RESEARCH AND DEVELOPMENT OF A NOVEL COMPACT SPACE WEATHER INSTRUMENTATION AND MEASUREMENTS (NEAT-SWIM). SPACE DYNAMICS LABORATORY (SDL) PROPOSES TO SUPPORT NASA GODDARD SPACE FLIGHT CENTER (GSFC) RESEARCHERS IN THEIR ONGOING EFFORTS TO DEVELOP NOVEL, COMPACT SPACE WEATHER INSTRUMENTATION. CURRENT TECHNOLOGIES OF INTEREST AIM TO PROVIDE ACCURATE IN SITU MEASUREMENTS OF THERMOSPHERIC AND IONOSPHERIC PARAMETERS BY ENERGY ANALYSIS, WHILE MINIMIZING DEMANDS ON SPACECRAFT RESOURCES. THE PRIMARY GOAL OF THIS COLLABORATIVE WORK IS TO ADVANCE THE TRL OF RELEVANT SENSORS, COMPONENTS, AND SUBASSEMBLIES TO ALLOW RAPID AND CREDIBLE RESPONSE TO ANNOUNCEMENTS OF SPACE WEATHER MISSION OPPORTUNITIES. TO THIS END, SDL WILL ASSIST IN THE DEVELOPMENT, CHARACTERIZATION, TEST, AND CALIBRATION OF A VARIETY OF ENABLING SENSOR TECHNOLOGIES. SDL WILL PERFORM FULL-FOV LABORATORY CALIBRATION OF THE ANDE FLIGHT SPARE WIND AND TEMPERATURE SPECTROMETER (WATS) IN ITS ION OPTICS TEST FACILITY. THE EXPERIMENTAL INVESTIGATION WILL PROVIDE A DETAILED COMPARISON OF CURRENT ION OPTICS SIMULATION PREDICTIONS WITH EXPECTED THERMOSPHERIC MEASUREMENT PERFORMANCE. SDL WILL COLLABORATE IN THE DEVELOPMENT OF PROMISING TECHNOLOGIES, AND CHARACTERIZE ENERGY ANALYZER DESIGN CANDIDATES THROUGH THEORETICAL AND EXPERIMENTAL WORK. SENSOR MODELING WILL BE PERFORMED USING SIMION ION TRAJECTORY CALCULATIONS AND MONTE CARLO SIMULATIONS. | UTAH STATE UNIVERSITY SPACE DYNAMICS LABORATORY | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 15, 2010 | Sep 15, 2010 | Sep 14, 2011 | ||
| AUTOMATED TOOL AND METHOD FOR SYSTEM SAFETY ANALYSIS TRIAKIS WILL PROVIDE SERVICES IN SUPPORT OF NASA SOFTWARE ASSURANCE RESEARCH PROGRAM (SARP) CENTER INITIATIVE RESEARCH PROJECT: AUTOMATED TOOL AND METHOD FOR SYSTEM SAFETY ANALYSIS. THESE SERVICES INCLUDE DEVELOPMENT OF AN ORION ORDINANCE SUBSYSTEM SIMULATION AND VIRTUAL INTEGRATION TEST FRAMEWORK THAT RE-USES MODEL INFORMATION EXTRACTED BY NASA TOOLS THAT ARE BEING DEVELOPED IN THE PROJECT. THE WORK IN 2010 FOCUSES ON AUTOMATION OF MANUAL METHODS THAT HAVE BEEN DEVELOPED TO MAP THE EXTRACTED MODEL INFORMATION TO THE SIMULATION MODEL FOR INTEGRATION TESTING. THIS EFFORT IS A CONTINUATION OF WORK WHICH STARTED THREE YEARS AGO. IN THE PAST PROCUREMENTS, TRIAKIS REVIEWED NASA S CREW EXPLORATION VEHICLE (CEV) PRELIMINARY HAZARD ANALYSIS (PHA), MADE RECOMMENDATIONS ON CANDIDATE CASES COMPATIBLE WITH VSIL-BASED TESTING AND SUPPORTED THE DEVELOPMENT OF TECHNIQUE/TOOL FOR CONVERTING TEXT-BASED REQUIREMENTS TO ICOSIM AUTO-TEST AND AUTO-TEST COMPATIBLE FORM. TRIAKIS ALSO DEVELOPED CEV SYSTEM-LEVEL VSIL SIMULATOR WITH ENOUGH FIDELITY TO CONDUCT LIMITED TESTING OF SELECTED CASES AS WELL AS EVALUATED VIABILITY OF SYSTEM-LEVEL TESTING USING OUTPUT OF REQUIREMENTS CONVERSION TOOL. | TRIAKIS CORPORATION | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541990All Other Professional, Scientific, and Technical Services | AR34 | Mar 1, 2010 | Mar 2, 2010 | Feb 28, 2011 | ||
| SUPPORT SERVICES TO POWER DISTRIBUTION EFFORTS, ARES | Curtiss-Wright DS, Inc. | $44,923 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 336419Other Guided Missile and Space Vehicle Parts and Auxiliary Equipment Manufacturing | AR34 | Jan 6, 2010 | Jan 6, 2010 | Jan 11, 2011 | ||
| THE RP-TOF PROJECT IS A COLLABORATION BETWEEN GSFC, JHU/APL, AND CREARE. THE RP-TOF PROJECT SEEKS TO DEVELOP A NEW MINIATURE SPACE FLIGHT MASS SPECTROMETER PROTOTYPE, BASED ON PRIOR INSTRUMENTS AND DESIGNS, SOME OF WHICH HAVE BEEN IN COLLABORATION WITH CREARE, INC. THE RP-TOF WILL BE A VERY COMPACT INSTRUMENT FOR ANALYSIS OF THE CHEMICAL COMPOSITION OF ROCKS, DUST, AND ICES ON PLANETS SUCH AS MARS, THE MOON, OR OTHER PLANETARY SATELLITES. A NEW ASPECT TO BE PURSUED IS THE ABILITY TO SWITCH BETWEEN ION POLARITIES (POSITIVE AND NEGATIVE) TO ENABLE BROADER CHARACTERIZATION OF SPECIES WITH BIASES FOR FORMING CATIONS OR ANIONS. IN ADDITION, THE INSTRUMENT WILL BE PACKAGED IN A SINGLE CYLINDRICAL HOUSING THAT INCLUDES A HIGH VACUUM PUMP TO BE DEVELOPED BY CREARE. THIS IS A CRITICAL ENABLING TECHNOLOGY FOR THIS TYPE OF INSTRUMENT, WHEN DEPLOYED IN ENVIRONMENTS WITH SUBSTANTIAL ATMOSPHERES (EARTH, MARS, TITAN) AS WELL AS IN COMBINED INSTRUMENTS USING GAS PROCESSING. IN BOTH CASES A HIGH-THROUGHPUT PUMP OF THE TYPE DEVELOPED AND MINIATURIZED BY CREARE IS REQUIRED TO PROCESS PERIODICAL GAS LOADING WHILE STILL ACHIEVING LOW BASE ANALYZER PRESSURE. THE CONTRACTOR WILL BE RESPONSIBLE FOR THE ANALYSIS, DESIGN, DEVELOPMENT, TEST, AND DELIVERY OF A TURBOMOLECULAR-DRAG PUMP AND CONTROLLER, WITH PUMPING PARAMETERS AND HOUSING CUSTOMIZED TO THE RP-TOF. CREARE WILL ADDITIONALLY EXAMINE THE OPERATIONAL ISSUES OF THE RP-TOF VACUUM SYSTEM AS IT WOULD BE DEPLOYED ON MARS OR ON TITAN. IN THE CASE OF TITAN, CREARE WILL CONDUCT A PRELIMINARY INVESTIGATION OF ENGINEERING SOLUTIONS TO THE HIGH AMBIENT PRESSURE CHALLENGE, INCLUDING POSSIBLE COMBINED TURBO-PUMP AND MECHANICAL BACKING PUMP SYSTEMS THAT COULD OPERATE BETWEEN HIGH VACUUM AND 1.5 BAR. AFTER A PERIOD OF INSTRUMENT TESTING AT GSFC, CREARE WILL CONDUCT LIMITED LIFETIME (CONTINUOUS AND START/STOP) TESTS OVER SEVERAL MONTHS, THEN RETURN THE PUMP TO GSFC. CREARE WILL ALSO SUPPORT DEVELOPMENT OF CONCEPTS FOR A FULL PUMPING SYSTEM FOR TITAN S SURFACE. | CREARE LLC | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541712 | AR34 | Sep 30, 2009 | Oct 1, 2009 | Sep 30, 2010 | ||
| GLOBAL PRECIPITATION MEASUREMENT MAGNETIC TORQUER BAR FLIGHT UNITS. THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA), THE OFFICE OF SPACE SCIENCE (OSS) AND THE GODDARD SPACE FLIGHT CENTER (GSFC) HAVE THE STATED MISSION TO DESIGN, DEVELOP, INTEGRATE, LAUNCH, AND OPERATE THE GLOBAL PRECIPITATION MEASUREMENT (GPM) MISSION. THE GPM MISSION IS ONE OF THE NEXT GENERATION SATELLITE-BASED EARTH SCIENCE CONSTELLATION MISSIONS THAT WILL STUDY GLOBAL PRECIPITATION (RAIN, SNOW AND ICE). THE GPM CORE OBSERVATORY WILL BE CARRYING BOTH A DUAL FREQUENCY RADAR INSTRUMENT AND A PASSIVE MICROWAVE RADIOMETER. THE CORE OBSERVATORY WILL SERVE AS A CALIBRATION STANDARD FOR THE OTHER MEMBERS OF THE GPM CONSTELLATION. | ITHACO SPACE SYSTEMS, INC. | $241,704 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 334511Search, Detection, Navigation, Guidance, Aeronautical, and Nautical System and Instrument Manufacturing | AR34 | Jun 16, 2009 | Jun 16, 2009 | Mar 18, 2011 | ||
| SOLAR DYNAMICS OBSERVATORY (SDO) GROUND SYSTEM OPERATIONAL READINESS EVALUATION - THE CONTRACTOR SHALL OBSERVE AND CRITIQUE THE SDO GROUND SYSTEMS PERFORMANCE DURING THE EXECUTION OF SDO MISSION SIMULATIONS. A SUMMARY REPORT WILL BE PROVIDED TO THE SDO GROUND SYSTEM MANAGER FOR EACH SIMULATION, THEN A WRAP-UP `SUMMARY AND ASSESSMENT REPORT AT THE CONCLUSION OF THE FOUR SIMULATIONS. | QWALTEC INC | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541330Engineering Services | AR34 | Apr 22, 2009 | Apr 22, 2009 | Sep 30, 2009 | ||
| PROVIDE DISTRESS ALERTING SATELLITE SYSTEM (DASS) ANALYSIS | THE JOHNS HOPKINS UNIVERSITY APPLIED PHYSICS LABORATORY LLC | $54,979 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541710 | AR34 | Apr 21, 2009 | Apr 27, 2009 | Jun 30, 2009 | ||
| POLYSONIC WIND TUNNEL TESTING FOR ARES I | THE BOEING COMPANY | $1,466,100 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 488190Other Support Activities for Air Transportation | AR34 | Mar 31, 2009 | Mar 31, 2009 | Mar 30, 2010 | ||
| LRO MISSION REHEARSAL EVALUATION | QWALTEC INC | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | — | 541330Engineering Services | AR34 | Mar 27, 2009 | Mar 27, 2009 | May 30, 2009 | ||
| LDCM FAULT MONITORY ANALYSIS | QWALTEC INC | $151,981 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | AR34 | Nov 10, 2008 | Nov 10, 2008 | Oct 31, 2009 | ||
| SAP PURCHASE REQUISITION: 4200265357 | ATK SPACE SYSTEMS LLC | $2,692,398 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 30, 2008 | Sep 30, 2008 | Sep 8, 2009 | ||
| SAP PURCHASE REQUISITION: 4200265340 | COMTECH AEROASTRO, INC | $699,386 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 30, 2008 | Sep 30, 2008 | Mar 13, 2009 | ||
| MICROSAT SYSTEMS, INC.(BAA ORS-08-03) - REFERENCE DESIGN FOR A LEO MODULAR, MULTI-MISSION SPACECRAFT BUS AND ASSOCIATED SERVICES. | MICROSAT SYSTEMS, INC. | $2,699,949 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 23, 2008 | Sep 23, 2008 | Nov 30, 2009 | ||
| GLORY MISSION OPERATIONS REHEARSAL DEVELOPMENT | QWALTEC INC | $114,732 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | AR34 | Sep 15, 2008 | Sep 15, 2008 | Jan 31, 2010 | ||
| SBIR PHASE III FOR TESS PHASE I SUPPORT STUDIES | ESPACE INC. | $149,066 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 11, 2008 | Sep 11, 2008 | Jun 11, 2009 | ||
| SPACECRAFT BUS | ATK SPACE SYSTEMS LLC | $140,119 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR34 | Sep 4, 2008 | Sep 4, 2008 | Apr 30, 2009 |