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Federal Contract Awards

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Award ID
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692M1520P00100
SERVICES SUPPORTING THE BIRD DETECTION MITIGATION FLIGHT TESTS.WHIRLWIND AVIATION, INC$168,500FEDERAL AVIATION ADMINISTRATIONFEDERAL AVIATION ADMINISTRATION—541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)AR31Sep 24, 2020Sep 24, 2020Jan 12, 2022
19CS8018P0030
HUMANITARIAN AIR SUPPORT DUE TO TS NATEMISCELLANEOUS FOREIGN AWARDEES$27,440STATE, DEPARTMENT OFAGENCY FOR INTERNATIONAL DEVELOPMENT—624230Emergency and Other Relief ServicesAR31Oct 24, 2017Oct 24, 2017Dec 5, 2017
19CS8018P0028
HUMANITARIAN AIR SUPPORT DUE TO TS NATEMISCELLANEOUS FOREIGN AWARDEES$52,500STATE, DEPARTMENT OFAGENCY FOR INTERNATIONAL DEVELOPMENT—624230Emergency and Other Relief ServicesAR31Oct 24, 2017Oct 24, 2017Oct 25, 2017
19CS8018P0010
HUMANITARIAN AIR SUPPORTMISCELLANEOUS FOREIGN AWARDEES$15,910STATE, DEPARTMENT OFAGENCY FOR INTERNATIONAL DEVELOPMENT—624230Emergency and Other Relief ServicesAR31Oct 24, 2017Oct 24, 2017Dec 5, 2017
19CS8018P0031
HUMANITARIAN AIR SUPPORT DUE TO THE TS. NATEMISCELLANEOUS FOREIGN AWARDEES$52,670STATE, DEPARTMENT OFAGENCY FOR INTERNATIONAL DEVELOPMENT—624230Emergency and Other Relief ServicesAR31Oct 24, 2017Oct 24, 2017Oct 25, 2017
NNG14HZ23P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.L3HARRIS TECHNOLOGIES, INC.$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Feb 25, 2015
NNG14HZ32P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.NORTHROP GRUMMAN SYSTEMS CORP$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Mar 15, 2015
NNG14HZ22P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.BAE SYSTEMS SPACE & MISSION SYSTEMS INC.$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Mar 15, 2015
NNG14HZ24P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.BAE SYSTEMS SPACE & MISSION SYSTEMS INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Feb 25, 2015
NNG14HZ31P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.LOCKHEED MARTIN INTEGRATED SYSTEMS, LLC$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Mar 15, 2015
NNG14HZ25P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.BAE SYSTEMS SPACE & MISSION SYSTEMS INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Feb 25, 2015
NNG14HZ26P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.RAYTHEON COMPANY$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Mar 15, 2015
NNG14HZ27P
IGF::OT::IGF SUSTAINABLE LAND IMAGING (SLI) - REDUCED INSTRUMENT ENVELOPE STUDY: THE CONTRACTOR SHALL PERFORM ONE OR MORE CONCEPTUAL DESIGNS OF IMAGER INSTRUMENTS TARGETING A REDUCED VOLUME, MASS, AND POWER ENVELOPE THAT CAN SATISFY LAND IMAGING PERFORMANCE REQUIREMENTS AND MEET NPR 8705.4 RISK CLASS B STANDARDS. THE CONTRACTOR SHALL ASSUME THE CONCEPT OF OPERATIONS FOR THE INSTRUMENT. THE CONTRACTOR SHALL PROVIDE IMAGING ALL LAND AND COASTAL AREA IN THE INSTRUMENTS FIELD OF VIEW, EVERY ORBIT. THE CONTRACTOR SHALL ASSUME AGILITY, MECHANICAL INTERFACE TO S/C, THERMAL INTERFACE TO S/C, AND ELECTRICAL INTERFACE TO SPACECRAFT (S/C). AS PART OF THIS DESIGN, THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING AT A MINIMUM SLI PERFORMANCE REQUIREMENTS TO IDENTIFY THE DRIVERS FOR MASS, VOLUME, AND POWER, AND COST FOR FUTURE MID-TERM INSTRUMENT DESIGNS. THE CONTRACTOR SHALL PROVIDE A DETAILED ASSESSMENT OF OPTICAL DESIGN AND FOCAL PLANE PERFORMANCE RELATIVE TO SLI PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL PERFORM ANALYSIS AND PROVIDE STUDY PRODUCTS ADDRESSING EMERGING TECHNOLOGIES AND TECHNIQUES TO FURTHER ENABLE IMPLEMENTATION EFFICIENCIES AND A SCHEDULE FOR POTENTIAL INFUSION INTO SLI. THE CONTRACTOR SHALL ACCOMMODATE ON-BOARD REFLECTIVE AND THERMAL BAND CALIBRATION SOURCES TO SATISFY PERFORMANCE REQUIREMENTS. THE CONTRACTOR SHALL DISCUSS CALIBRATION APPROACH AND DEVELOP A CALIBRATION ERROR BUDGET. THE CONTRACT SHALL ASSESS THERMAL CONTROL, INCLUDING TECHNIQUES AND TECHNOLOGIES FOR DETECTOR COOLING AND STABILIZATION, ACCOMMODATION OF POTENTIALLY LARGE RADIATOR AREAS ON A SMALLSAT PLATFORM, ASSESSMENT OF PASSIVE VS. ACTIVE COOLING ON A SMALLSAT PLATFORM. THE CONTRACTOR SHALL IDENTIFY SPACECRAFT INTERFACE ASSUMPTIONS, INCLUDING THOSE FOR ATTITUDE CONTROL AND LINE OF SIGHT STABILITY, AND RATIONALE FOR SATISFYING IMAGING REQUIREMENTS. THE CONTRACTOR SHALL DELIVER BRIEF MONTHLY UPDATED STATUS PACKAGES. THE CONTRACTOR SHALL HOST A KICKOFF MEETING. THE CONTRACTOR SHALL SUPPORT A PRELIMINARY RESULTS (MIDTERM) REVIEW. THE CONTRACTOR SHALL HOST A FINAL RESULTS REVIEW. SPECIFIC ACTIVITIES SHALL BE PRIMARILY PERFORMED AT THE CONTRACTOR S LOCATION.SURREY SATELLITE TECHNOLOGY US LLC$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Aug 25, 2014Aug 25, 2014Mar 15, 2015
NNC12CA45C
IGF::OT::IGF HIGH POWER, HIGH EFFICIENCY Q-BAND (37.0 TO 42.0 GHZ) SPACE TRAVELING WAVE TUBE (TWT) LEADING TO THE DEVELOPMENT OF A SATELLITE TRANSPONDER FOR RF PROPAGATION STUDIESSTELLANT SYSTEMS INC$500,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR31Oct 12, 2012Oct 12, 2012Mar 5, 2018
N0017311C2054
NEW AWARD FOR RESEARCH AND DEVELOPMENT OF A PROTOTYPE ROBOTIC ARM FOR NANOSATELLITESTETHERS UNLIMITED, INC.$199,999DEFENSE CONTRACT MANAGEMENT AGENCY (DCMA)DEPT OF THE NAVY—541712AR31Sep 30, 2011Sep 30, 2011Nov 16, 2012
NNJ11HA36P
IMPROVED GLOVE BLADDER RESTRAINT ASSEMBLY THE SPACE SUIT PRESSURE GARMENT REQUIRES INNOVATIVE TECHNOLOGIES THAT INCREASE THE LIFE, COMFORT, MOBILITY AND DURABILITY OF THE SPACE SUIT GLOVES FOR FUTURE NASA MISSIONS. IN ORDER TO ACHIEVE THESE ADVANCES, NASA DESIRES TO EXPLORE NONTRADITIONAL APPROACHES TO SPACE SUIT GLOVE DESIGN. SPECIFIC AREAS OF INTEREST INCLUDE METACARPAL JOINT, THUMB JOINT, AND PALM DESIGN. GLOVE FIT IS ALSO CRITICAL TO PERFORMANCE, AND SHOULD BE AN IMPORTANT CONSIDERATION IN GLOVE DESIGN. THIS CONTRACT INVOLVES THE GENERATION AND DOWN SELECT OF CONCEPTS IN FOUR DIFFERENT GLOVE DESIGN AREAS, INCORPORATION OF THE SELECTED CONCEPTS INTO PROTOTYPE GLOVES, DOWN SELECT TO A SINGLE GLOVE DESIGN, AND FABRICATION, PRE-DELIVERY TESTING AND DELIVERY OF TWO PAIRS OF THE FINAL GLOVE BLADDER/RESTRAINT ASSEMBLY DESIGN. AFTER ACHIEVING A THOROUGH UNDERSTANDING OF THE DESIGN REQUIREMENTS SET FORTH IN THIS CONTRACT AND HAVING CONDUCTED SUFFICIENT RESEARCH OF PAST AND CURRENT GLOVE DESIGNS FOR PRESSURE GARMENTS, THE CONTRACTOR SHALL GENERATE MULTIPLE DESIGN MODIFICATION CONCEPTS THAT IMPROVE UPON EXISTING GLOVE DESIGNS AND MEET THE REQUIREMENTS PROVIDED IN APPENDIX A OF THE SOW. THE CONTRACTOR SHALL BEGIN WITH THE EXISTING GLOVE DESIGN, AND GENERATE A MINIMUM OF THREE (3) CONCEPTS FOR IMPROVEMENT IN EACH OF THE FOLLOWING AREAS OF INTEREST: A. BLADDER DESIGN B. METACARPAL JOINT DESIGN C. PALM DESIGN D. FINGER LENGTH SIZING THE CONTRACTOR SHALL COMPLETE THE DETAILED DESIGN AND FABRICATION OF PROTOTYPES USING THE CONCEPTS SELECTED IN TASK 1 OF THE SOW. THE CONTRACTOR SHALL PRESENT THEIR PROTOTYPES TO THE GOVERNMENT AT THE CONTRACTOR S FACILITY DURING A PROTOTYPE REVIEW AND DOWN SELECT. THE CONTRACTOR SHALL COMPLETE ANY FINAL DESIGN MODIFICATIONS AS WELL AS FABRICATION OF TWO (2) PAIRS OF THE FINAL GLOVE BLADDER/RESTRAINT ASSEMBLY DESIGN USING THE COMPONENT CONCEPTS SELECTED IN TASK 2 OF THE SOW. THE CONTRACTOR SHALL GENERATE A TEST PLAN AND CONDUCT TESTING TO VERIFY THAT ALL REQUIREMENTS HAVE BEEN MET. AFTER ALL FABRICATION IS COMPLETE AND HARDWARE HAS PASSED REQUIREMENTS VERIFICATION TESTING, THE CONTRACTOR SHALL SHIP THE DELIVERABLES TO JSC, BLDG. 7 BOND PRIOR TO THE FINAL HARDWARE DELIVERY PRESENTATION. NASA WILL HAVE THIRTY (30) BUSINESS DAYS TO COMPLETE ACCEPTANCE TESTING ON THE DELIVERED HARDWARE.FLAGSUIT LLC$159,833NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—315992AR31Jan 10, 2011Jan 11, 2011Aug 26, 2011
NNM11AA27T
SOLICITATION TO CONTINUE MSFC SPECIALIZED ENGINEERING SUPPORT BY THE SAME CONTRACTOR. THE CONTRACTOR CHANGED THEIR COMPANY NAME; THEREFORE A NEW TASK ORDER NUMBER WILL BE ISSUED WITH THE NEW NAME.LEIDOS, INC.$2,292,924NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541330Engineering ServicesAR31Dec 21, 2010Dec 25, 2010Jul 31, 2012
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THIS TASK ORDER IS TO CONTINUE MSFC SPECIALIZED ENGINEERING SUPPORT BY THE SAME CONTRACTOR. THE CONTRACTOR CHANGED THEIR COMPANY NAME; THEREFORE A NEW TASK ORDER NUMBER WILL BE ISSUED WITH THE NEW NAME. THE CONTRACTOR SHALL PROVIDE ENGINEERING SUPPORT TO THE MARSHALL SPACE FLIGHT CENTER (MSFC) ENGINEERING DIRECTORATE INCLUDING BUT NOT LIMITED TO THE DESIGN, DEVELOPMENT AND DEFINITION OF THE FLIGHT CONTROL SYSTEM, GUIDANCE, NAVIGATION, AND SEPARATION SYSTEMS IN SUPPORT OF SPACECRAFT AND LAUNCH VEHICLES INCLUDING SYSTEM AND SUBSYSTEM REQUIREMENTS AND SPECIFICATIONS. THE CONTRACTOR SUPPORT SHALL INCLUDE BUT IS NOT LIMITED TO MATHEMATICAL MODELING, COMPUTER SIMULATION, ALGORITHM DEVELOPMENT, CODE DEVELOPMENT, ASCENT AND REENTRY FLIGHT DYNAMICS ANALYSIS, COUPLED FREQUENCY AND TIME DOMAIN STABILITY CONTROL SYSTEM ANALYSIS, AERODYNAMICS ANALYSIS, MANUAL STEERING CONCEPT EVALUATION, SIMULATION VISUALIZATION SUPPORT, FLIGHT CONTROL SYSTEM AND FILTER DESIGN AND PERFORMANCE OPTIMIZATIONS, GUIDANCE AND NAVIGATION ARCHITECTURE DESIGN AND ANALYSIS SUPPORT AND MULTI-BODY VEHICLE FLIGHT SEPARATION DYNAMICS ANALYSIS. THE CONTRACTOR SHALL PARTICIPATE IN REQUIREMENT REVIEWS, TECHNICAL MEETINGS AND WORKING GROUPS AS WELL AS SUPPORT THE DEVELOPMENT OF PRESENTATION AND DOCUMENTATION DATA.LEIDOS, INC.$1,870,453NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541330Engineering ServicesAR31Dec 16, 2010Dec 25, 2010Jul 31, 2012
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HEAVY ION RADIATION TEST-THE NASA/JSC AVIONICS SYSTEMS DIV. PROVIDES RADIATION TEST PROCEDURES AND ANALYSIS OF ELECTRONIC FLIGHT HARDWARE. THE TESTING IS NECESSARY TO VERIFY THE OPERATION OF METAL OXIDE SEMICONDUCTOR FIELD EFFECT TRANSISTOR (MOSFET) COMPONENTS USED FOR THE ORION PROGRAM. TESTING WITH HIGH ENERGY HEAVY IONS TO A PARTICULAR DEPTH IS NECESSARY TO DETERMINE THE USABILITY OF MOSFETS FOR THE LUNAR ENVIRONMENT. RESULTS FROM THIS TESTING IS USED TO CALCULATE THE ESTIMATED TIME BEFORE ABNORMAL BEHAVIOR OR A CRITICAL FAILURE CAN BE EXPECTED TO OCCUR IN LUNAR ENVIRONMENTS. THIS RADIATION TEST WILL PROVIDE THE DATA THAT DETERMINES THE SPACE FLIGHT ACCEPTABILITY OF A CRITICAL PART TO THE DESIGN OF THE ORION POWER AND DATA UNIT (PDU). IF THE PART IS FOUND TO BE ACCEPTABLE, THE DESIGN OF THE PDU CAN CONTINUE AND ENGINEERING UNITS WILL BE AVAILABLE TO SUPPORT THE INTEGRATED TESTING OF AVIONICS IN THE FIRST QUARTER OF FY11. IF THIS PART IS NOT ACCEPTABLE, THE PDU WILL NOT BE ABLE TO MEET ITS EXISTING SCHEDULE AND THE ORION PROJECT WILL HAVE TO EXECUTE CONTINGENCY PLANS. BY PERFORMING THIS TEST IN JUNE, THE ORION PROJECT WILL HAVE THE DATA NECESSARY TO EFFECTIVELY DECIDE HOW TO PROCEED WITH THE PDU DEVELOPMENT PLANS AND WITH THE DEVELOPMENT PLANS OF ALL THE OTHER HARDWARE THAT IS DEPENDENT ON THE PDUS. NO SPECIAL TESTING EQUIPMENT WILL BE PROVIDED UNDER THIS CONTRACT. THE HIGH ENERGY ION BEAM AT CYCLOTRON INSTITUTE (CI) AT TEXAS A&M HAS BEEN USED FOR TESTING FOR INDIVIDUAL ELECTRONIC PARTS FOR MANNED PROGRAMS PREVIOUSLY BY NASA. THIS PROCUREMENT WILL PROVIDE THE TEST FACILITY, THE HIGH-ENERGY HEAVY ION BEAM, THE NECESSARY DOSIMETRY, AND REQUIRED OPERATIONS PERSONNEL NEEDED FOR THE TESTING ON A RATE PER HOUR BASIS.TEXAS A & M UNIVERSITY$70,380NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—611310Colleges, Universities, and Professional SchoolsAR31Jun 8, 2010Jun 8, 2010Sep 30, 2010
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CONNECT SOFTWARE REQUIREMENTS REVIEW BOARD CHAIRALPHAPORT INC$11,623NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541330Engineering ServicesAR31Nov 3, 2008Nov 3, 2008Dec 31, 2008
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ACME MECHANICAL SUPPORTALPHAPORT INC$33,733NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541330Engineering ServicesAR31Nov 3, 2008Nov 3, 2008Dec 31, 2008
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MSFC UPPER STAGE PDR REVIEW TEAM LEADALPHAPORT INC$77,165NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541330Engineering ServicesAR31Oct 20, 2008Jun 3, 2008Oct 31, 2008
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WRAP AROUND AIRBAGS FOR POST LANDING RECOVERY TESTILC DOVER LP$12,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541710AR31Oct 14, 2008Oct 14, 2008Apr 4, 2011
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GENERATION 1 WRAP-AROUND AIR BAGS. THE OBJECTIVE OF THE WORK DESCRIBED IN THIS TASK ORDER IS TO DESIGN AND BUILD FULL-SCALE GEN 1 WRAP-AROUND AIR BAGS SUITABLE FOR DROP-TESTING BY NASA. THE INTENT OF THESE DROP TESTS IS TO VERIFY BASIC WAAB PERFORMANCE PREDICTIONS FROM THE LS DYNA ANALYSIS. THESE TESTS ARE NOT INTENDED TO VERIFY THAT THE WRAP-AROUND AIR BAG DESIGN PROVIDES ADEQUATE PERFORMANCE FOR ALL LANDING CONDITIONS, OR TO VERIFY THE STRUCTURAL INTEGRITY OF THE AIR BAGS. IN ORDER TO MEET THE TEST OBJECTIVES AND MINIMIZE SCHEDULE, IT IS NASA S EXPECTATION THAT THE GEN 1 WAAB DESIGN MAY BE VERY SIMILAR TO THE PREVIOUSLY FABRICATED WAAB PROTOTYPE WITH SOME MODIFICATIONS RESULTING FROM: A) LESSONS LEARNED FROM THE PROTOTYPE FABRICATION AND DEPLOYMENT TESTING; AND B) PREVIOUS AND/OR ON-GOING WAAB DESIGN OPTIMIZATION ACTIVITIES. THE GEN 1 WAAB ACTIVITY DESCRIBED IN THIS SOW IS ONE OF FOUR INDIVIDUAL AIR BAG DEVELOPMENT TASKS THAT NASA IS PLANNING TO CONDUCT. THE FOUR AIR BAG DEVELOPMENT TASKS ARE LISTED BELOW AND ARE PLANNED TO BE PHASED APPROXIMATELY AS SHOWN IN FIGURE 1.ILC DOVER LP$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AR31Sep 29, 2008Sep 29, 2008May 15, 2009
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SAP PURCHASE REQUISITION: 4200267476 GEN 2 AIRBAG POST-TEST ANALYSIS AND REPORTINGILC DOVER LP$50,593NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541710AR31Sep 26, 2008Sep 26, 2008Feb 27, 2009
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