Coronavirus Contracts

Donate
Contracts Vendors Agencies Categories States
Coronavirus Contracts
Tracking Federal Purchases to Fight the Coronavirus
Search contract descriptions, companies and agencies.
Home › All Categories › Category ›
Aeronautics/Space Technology Basic Research R&D
Total Committed Value of Federal Contracts
$84.2M
Total Contracts
7
Total Actions
33

Recent Contract Actions

Contracts can have multiple “contract actions”: This is how agencies spend money for a specific purpose, adjust the amount committed or change the contract in a way that doesn’t affect the amount. That last scenario is usually indicated by a $0 action. If there is a contract action for a negative amount, it generally means the contract was adjusted or canceled.

Description Vendor Agency Effective Estimated completion Amount Committed
COVID-19 SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC) BOEING COMPANY, THE National Aeronautics and Space Administration October 16, 2019 November 15, 2021 $0
COVID-19 PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT. THE BOEING COMPANY National Aeronautics and Space Administration September 01, 2007 December 31, 2025 $0
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT. THE BOEING COMPANY National Aeronautics and Space Administration September 01, 2007 December 31, 2025 $84,109,481
SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC) BOEING COMPANY, THE National Aeronautics and Space Administration October 16, 2019 November 15, 2021 $0
COVID-19 (OMB MEMO M-20-22)TOPOLOGY OPTIMIZATION OF WIND TUNNEL BALANCE AXIAL SECTION. WIND TUNNEL FORCE BALANCES HAVE BEEN USED FOR OVER A CENTURY TO HELP AERODYNAMICISTS PREDICT FORCES AND MOMENTS EXERTED ON AIRCRAFT AND THEY CONTINUE TO REMAIN THE PRIMARY FORCE MEASUREMENT DEVICES USED DURING WIND TUNNEL TESTING. FORCE BALANCES PROVIDE THE CONNECTION BETWEEN THE WIND TUNNEL MODEL AND THE STING THAT IS USED TO SUSPEND THE MODEL IN THE TUNNEL FLOW. THEREFORE, BALANCES PERFORM TWO IMPORTANT BUT COMPETING OBJECTIVES: 1) SAFELY SUPPORT THE WIND TUNNEL MODEL THROUGHOUT THE TUNNEL TEST, 2) ACCURATELY RESOLVING THE FORCES AND MOMENTS EXERTED ON THE AIRCRAFT, WHICH REQUIRES SUFFICIENT RESOLUTION AND A MATHEMATICAL MODEL. WIND TUNNEL FORCE BALANCES ARE EFFECTIVELY A COUPLING OF MANY SPRING ELEMENTS. THE SPRINGS HAVE BEEN DESIGNED FOR THE LOADS EXPECTED IN THE TEST. WHILE THERE ARE MANY APPROACHES TO MEASURING FORCE, IN THIS APPLICATION, THE SPRINGS BECOME TRANSDUCERS WITH THE APPLICATION OF STRAIN GAGES THAT PROVIDE ELECTRICAL FEEDBACK PROPORTIONAL TO THE APPLIED STRAIN EXPERIENCED BY THE STRAIN GAGE. THE PRIMARY OBJECTIVES OF THIS EFFORT ARE TO DEVELOP TOPOLOGY OPTIMIZATION CODE ATTEMPTING TO MEET THE FOUR DESIGN OPTIMIZATION OBJECTIVES AS OUTLINED IN THE STATEMENT OF WORK, AND TO DEVELOP A NOVEL APPROACH TO OPTIMIZING STRAIN GAGE PLACEMENT USING LOCAL VARIABLES WITHIN THE LARGER TRADITIONAL TOPOLOGY OPTIMIZATION GLOBAL VARIABLE OPTIMIZATION (FOR VON MISES STRESS FOR INSTANCE). NATIONAL INSTITUTE OF AEROSPACE ASSOCIATES National Aeronautics and Space Administration February 06, 2019 August 31, 2021 $0
COVID-19 (OMB MEMO M-20-22)DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC). EAGLE AVIATION TECHNOLOGIES, LLC National Aeronautics and Space Administration November 01, 2018 September 30, 2020 $0
COVID-19 (OMB MEMO M-20-22)DESIGN AND FABRICATION REQUIREMENTS FOR A ROTARY-WING TEST STAND FOR THE NASA ICING RESEARCH TUNNEL (IRT). CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
COVID-19 PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT. THE BOEING COMPANY National Aeronautics and Space Administration September 01, 2007 December 31, 2025 $0
COVID-19 FIRST DDT AND E, ARES I-X, AND FLIGHT TESTS. FIRST STAGE WILL BE A FIVE SEGMENT, SOLID ROCKET BOOSTER DERIVED FROM THE SPACE SHUTTLE PROGRAM (SSP) SOLID ROCKET BOOSTER (SRB)/REUSABLE SOLID ROCKET MOTOR (RSRM). THE CONTRACTOR SHALL FURNISH THE NECESSARY MANAGEMENT, ENGINEERING, LABOR, FACILITIES, TOOLS, EQUIPMENT, AND MATERIALS REQUIRED FOR FIRST STAGE DEVELOPMENT, QUALIFICATION, CERTIFICATION AND ACCEPTANCE PROGRAM. ACTIVITIES INCLUDE: REDESIGN AND TESTING OF THE MOTOR TO INCORPORATE THE FIFTH SEGMENT AND PRODUCTION OF FIVE FULL SCALE GROUND STATIC TEST MOTORS: TWO DEVELOPMENT MOTORS (DMS)-AND THREE QUALIFICATION MOTORS (QMS) STRUCTURAL TEST ARTICLE (STA), GROUND VIBRATION TEST MOTORS (GVTMS) AND OTHER DEVELOPMENT TESTING REDESIGN OF THE AVIONICS, DECELERATION, SEPARATION, AND FLIGHT TERMINATION SYSTEM (FTS) SUBSYSTEMS ARES I-X: SIMULATED ARES I OUTER MOLD LINE/MASS PROPERTIES USING MODIFIED SRB/RSRM AND THREE FLIGHT TEST VEHICLES. TAS::80 0124::TAS ATK LAUNCH SYSTEMS INCORPORATED National Aeronautics and Space Administration April 17, 2006 December 31, 2023 $0
COVID-19 SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC) BOEING COMPANY, THE National Aeronautics and Space Administration October 16, 2019 November 15, 2021 $0
DESIGN, ANALYSIS, AND FABRICATION OF NEW HARDWARE AND MODIFYING EXISTING SWASHPLATE OF THE ARMY ROTOR CONTROL SYSTEM (ARTS). CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
VACUUM SPIN STAND - DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC). ADVANCED TECHNOLOGIES, INC. National Aeronautics and Space Administration September 11, 2019 November 30, 2020 $0
SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC) BOEING COMPANY, THE National Aeronautics and Space Administration October 16, 2019 November 15, 2021 $0
FABRICATION AND DESIGN OF BOLD STEP TEST WIND TUNNEL MODEL. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
DESIGN, ANALYSIS, AND FABRICATION OF NEW HARDWARE AND MODIFYING EXISTING SWASHPLATE OF THE ARMY ROTOR CONTROL SYSTEM (ARTS). CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
DESIGN AND FABRICATION REQUIREMENTS FOR A ROTARY-WING TEST STAND FOR THE NASA ICING RESEARCH TUNNEL (IRT). THE TEST STAND WILL ALLOW FOR THE INSTALLATION AND MOUNTING OF ROTARY-WING VEHICLES AND COMPONENTS FOR ICING TESTS IN THE IRT. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
VACUUM SPIN STAND - DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC). ADVANCED TECHNOLOGIES, INC. National Aeronautics and Space Administration September 11, 2019 November 30, 2020 $0
DESIGN, ANALYZE FOR SAFETY, AND FABRICATE A HINGELESS BLADE SET TO BE USED WITH THE TILTROTOR AEROELASTIC STABILITY TESTBED (TRAST). EAGLE AVIATION TECHNOLOGIES, LLC National Aeronautics and Space Administration November 01, 2018 September 30, 2020 $0
VACUUM SPIN STAND - DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC). ADVANCED TECHNOLOGIES, INC. National Aeronautics and Space Administration September 11, 2019 November 30, 2020 $0
DESIGN, ANALYZE FOR SAFETY, AND FABRICATE A HINGELESS BLADE SET TO BE USED WITH THE TILTROTOR AEROELASTIC STABILITY TESTBED (TRAST). EAGLE AVIATION TECHNOLOGIES, LLC National Aeronautics and Space Administration November 01, 2018 September 30, 2020 $0
COMMON RESEARCH MODEL - DESIGN AND FABRICATION OF THE 10% ACOUSTICALLY TREATED-HIGH LIFT COMMON RESEARCH MODEL. THE NEW 10% AT-HL COMMON RESEARCH MODEL WILL BE TESTED AT NASA LANGLEY'S 14X22 FT. WIND TUNNEL. EAGLE AVIATION TECHNOLOGIES, LLC National Aeronautics and Space Administration November 01, 2018 September 30, 2020 $0
DESIGN AND FABRICATION REQUIREMENTS FOR A ROTARY-WING TEST STAND FOR THE NASA ICING RESEARCH TUNNEL (IRT). THE TEST STAND WILL ALLOW FOR THE INSTALLATION AND MOUNTING OF ROTARY-WING VEHICLES AND COMPONENTS FOR ICING TESTS IN THE IRT. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
FABRICATION AND DESIGN OF BOLD STEP TEST WIND TUNNEL MODEL. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
DESIGN, ANALYSIS, AND FABRICATION OF NEW HARDWARE AND MODIFYING EXISTING SWASHPLATE OF THE ARMY ROTOR CONTROL SYSTEM (ARTS). CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
FIRST DDT AND E, ARES I-X, AND FLIGHT TESTS. FIRST STAGE WILL BE A FIVE SEGMENT, SOLID ROCKET BOOSTER DERIVED FROM THE SPACE SHUTTLE PROGRAM (SSP) SOLID ROCKET BOOSTER (SRB)/REUSABLE SOLID ROCKET MOTOR (RSRM). THE CONTRACTOR SHALL FURNISH THE NECESSARY MANAGEMENT, ENGINEERING, LABOR, FACILITIES, TOOLS, EQUIPMENT, AND MATERIALS REQUIRED FOR FIRST STAGE DEVELOPMENT, QUALIFICATION, CERTIFICATION AND ACCEPTANCE PROGRAM. ACTIVITIES INCLUDE: REDESIGN AND TESTING OF THE MOTOR TO INCORPORATE THE FIFTH SEGMENT AND PRODUCTION OF FIVE FULL SCALE GROUND STATIC TEST MOTORS: TWO DEVELOPMENT MOTORS (DMS)-AND THREE QUALIFICATION MOTORS (QMS) STRUCTURAL TEST ARTICLE (STA), GROUND VIBRATION TEST MOTORS (GVTMS) AND OTHER DEVELOPMENT TESTING REDESIGN OF THE AVIONICS, DECELERATION, SEPARATION, AND FLIGHT TERMINATION SYSTEM (FTS) SUBSYSTEMS ARES I-X: SIMULATED ARES I OUTER MOLD LINE/MASS PROPERTIES USING MODIFIED SRB/RSRM AND THREE FLIGHT TEST VEHICLES. TAS::80 0124::TAS ATK LAUNCH SYSTEMS INCORPORATED National Aeronautics and Space Administration April 17, 2006 December 31, 2023 $0
THIS IS WORK IS FOR THE DETAILED DESIGN AND FABRICATION OF AN ADVANCED ROTORCRAFT TESTBED SUITABLE FOR TESTING A VARIETY OF WINGED COMPOUND ROTORCRAFT CONFIGURATIONS IN THE 14- BY 22-FOOT SUBSONIC TUNNEL BY WAY OF A TRAVERSING ASSEMBLY MOUNTED BELOW ADVANCED TECHNOLOGIES, INC. National Aeronautics and Space Administration September 11, 2019 November 30, 2020 $86,054
FABRICATION AND DESIGN OF BOLD STEP TEST WIND TUNNEL MODEL. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
COMMON RESEARCH MODEL - DESIGN AND FABRICATION OF THE 10% ACOUSTICALLY TREATED-HIGH LIFT COMMON RESEARCH MODEL. THE NEW 10% AT-HL COMMON RESEARCH MODEL WILL BE TESTED AT NASA LANGLEY'S 14X22 FT. WIND TUNNEL. EAGLE AVIATION TECHNOLOGIES, LLC National Aeronautics and Space Administration November 01, 2018 September 30, 2020 $0
DESIGN AND FABRICATION REQUIREMENTS FOR A ROTARY-WING TEST STAND FOR THE NASA ICING RESEARCH TUNNEL (IRT). THE TEST STAND WILL ALLOW FOR THE INSTALLATION AND MOUNTING OF ROTARY-WING VEHICLES AND COMPONENTS FOR ICING TESTS IN THE IRT. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
VACUUM SPIN STAND - DESIGN, ANALYSIS AND FABRICATION OF A NEW VACUUM SPIN STAND SUITABLE FOR TESTING ROTOR BLADES INSIDE THE NASA LANGLEY RESEARCH CENTER'S LANGLEY AEROTHERMODYNAMICS LABORATORY (LAL) 60-FT VACUUM SPHERE TEST CHAMBER (60VSTC). ADVANCED TECHNOLOGIES, INC. National Aeronautics and Space Administration September 11, 2019 November 30, 2020 $0
DESIGN AND FABRICATION REQUIREMENTS FOR A ROTARY-WING TEST STAND FOR THE NASA ICING RESEARCH TUNNEL (IRT). THE TEST STAND WILL ALLOW FOR THE INSTALLATION AND MOUNTING OF ROTARY-WING VEHICLES AND COMPONENTS FOR ICING TESTS IN THE IRT. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT. THE BOEING COMPANY National Aeronautics and Space Administration September 01, 2007 December 31, 2025 $0
FABRICATION AND DESIGN OF BOLD STEP TEST WIND TUNNEL MODEL. CALSPAN SYSTEMS CORPORATION National Aeronautics and Space Administration August 27, 2019 April 30, 2021 $0
About this data
This data comes from the Federal Procurement Data System, which includes all contracts worth $10,000 or more. We look at all contracts that are tagged with the procurement code for COVID-19 or otherwise started in 2020 and contain “COVID-19” in the description. Department of Defense contracting data is subject to a 90-day delay before it appears in the data.
Close Comment Creative Commons Donate Email Facebook Mobile Phone Podcast Print RSS Search Search Twitter WhatsApp
Current site Current page