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Award ID | Description | Recipient | Total Value | Awarding Agency | Funding Agency | Set Aside | NAICS | PSC | Award Date | Start Date | End Date | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CONTRACTOR TO PROVIDE RESEARCH REPORTS ON STUDIES ABOUT HOW TO MAKE MARS ASCENT VEHICLE LIGHTER AND MORE EFFICIENT. | AEROJET ROCKETDYNE OF DE, INC | $717,605 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Jul 12, 2024 | Jul 17, 2024 | Oct 15, 2024 | ||
| NEXT GENERATION ADDITIVELY MANUFACTURED EXHAUST CONTROL DUCT ENABLING HYPERSONIC AFFORDABILITY | AEROJET ROCKETDYNE OF DE, INC | $1,649,958 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AC12NATIONAL DEFENSE R&D SERVICES; DEPARTMENT OF DEFENSE - MILITARY; APPLIED RESEARCH | Nov 22, 2022 | Nov 22, 2022 | Apr 30, 2025 | ||
| NEW START EW-201341 | AEROJET ROCKETDYNE OF DE, INC | $24,962 | DEPT OF THE ARMY | DEPT OF THE ARMY | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AJ12GENERAL SCIENCE AND TECHNOLOGY R&D SERVICES; GENERAL SCIENCE AND TECHNOLOGY; APPLIED RESEARCH | Jan 28, 2021 | Jan 26, 2020 | Dec 31, 2021 | ||
| ENGINEERING DOCUMENTATION FORMAT CONVERSION FROM MICRO-FILM TO ELECTRONIC VERSION ENGINEERING SUPPORT FOR ENGINE DISASSEMBLY PROCESS DEVELOPMENT | AEROJET ROCKETDYNE OF DE, INC | $157,449 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AR71 | Jun 25, 2020 | Jul 1, 2020 | Sep 30, 2020 | ||
| R&D TRADE STUDY TO REDESIGN THE XLR-132 PUMP-FED STORABLE ENGINE | AEROJET ROCKETDYNE OF DE, INC | $9,421,073 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR12SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; APPLIED RESEARCH | Jun 25, 2020 | Jul 1, 2020 | Apr 30, 2021 | ||
| NASA HUMAN LANDING SYSTEM (HLS) REFUELING ELEMENT - CONTRACTOR SHALL REFINE THE ARCHITECTURE, FUNCTIONAL ALLOCATION OPTIONS AND COMMON INTERFACES REQUIRED TO ENABLE THE HLS TO PROVIDE HUMAN LANDING CAPABILITY; INFORM OVERALL HLS REQUIREMENTS, PROVIDE UNDERSTANDING OF ELEMENT DESIGNS, SCHEDULES AND COSTS; IDENTITY KEY ELEMENT TECHNOLOGY MATURATION AREAS, AND IMPLEMENT DESCENT TECHNOLOGY MATURATION PLANS; IDENTIFY ANY LONG-LEAD PROCUREMENT ITEMS | AEROJET ROCKETDYNE OF DE, INC | $888,683 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AZ12 | May 30, 2019 | May 30, 2019 | Dec 20, 2019 | ||
| PRESSURE GAIN PROPULSION (PGP) RAMJET DEMONSTRATION | AEROJET ROCKETDYNE OF DE, INC | $8,852,497 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 541715Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology) | AC12NATIONAL DEFENSE R&D SERVICES; DEPARTMENT OF DEFENSE - MILITARY; APPLIED RESEARCH | Sep 27, 2018 | Sep 27, 2018 | Jun 24, 2024 | ||
| POST AWARD CONFERENCE FOR UUV FAMILY OF SERVICES | AEROJET ROCKETDYNE OF DE, INC | $2,500 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 336999All Other Transportation Equipment Manufacturing | 1940SMALL CRAFT | Aug 6, 2018 | Aug 6, 2018 | Sep 30, 2018 | ||
| HLACS PLATELET STACK/PLATELET INJECTOR | AEROJET ROCKETDYNE OF DE, INC | $4,999,999 | MISSILE DEFENSE AGENCY (MDA) | MISSILE DEFENSE AGENCY (MDA) | — | 336419Other Guided Missile and Space Vehicle Parts and Auxiliary Equipment Manufacturing | 1420GUIDED MISSILE COMPONENTS | Aug 28, 2017 | Aug 28, 2017 | May 31, 2019 | ||
| IGF::OT::IGF TASK ORDER NNC16TA65T FOR LOW ENRICHED URANIUM ENGINE AND COST ANALYSIS. | AEROJET ROCKETDYNE OF DE, INC | $7,557,287 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH | Aug 5, 2016 | Aug 4, 2016 | Aug 31, 2021 | ||
| IGF::OT::IGF: B TEST STAND LH&LOX DOCK CONTROL PANELS | AEROJET ROCKETDYNE OF DE, INC | $273,806 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | C222ARCHITECT AND ENGINEERING- GENERAL: ELECTRICAL SYSTEMS | Jul 7, 2016 | Jul 7, 2016 | Apr 7, 2017 | ||
| IGF::OT::IGF GRIFFIN | AEROJET ROCKETDYNE OF DE, INC | $594,966 | DEPT OF THE AIR FORCE | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541712 | AC61 | Apr 27, 2016 | Apr 27, 2016 | Jun 14, 2018 | ||
| IGF::OT::IGF TASK ORDER NNC16TA03T FOR FREEJET TESTING OF A DUAL MODE RAMJET (DMRJ) AT LOW MACH CONDITIONS. THE OVERALL OBJECTIVE OF THIS WORK IS TO CONDUCT A SUBSCALE 3X FREE-JET TEST USING THE AR 3RD GENERATION FLOWPATH ARCHITECTURE INTEGRATED WITH PRE-EXISTING FACET INLET, NOZZLE AND PEDESTAL HARDWARE. THE TEST WILL BE CONDUCTED IN NASA LANGLEYS 8-FT HIGH TEMPERATURE TUNNEL (HTT) BETWEEN MACH 2 AND MACH 4 FLIGHT CONDITIONS IN ORDER TO ASSESS PERFORMANCE AND OPERABILITY AND TO VALIDATE DESIGN TOOLS. THE CONTRACTOR SHALL BE RESPONSIBLE FOR THE DESIGN, MANUFACTURE AND TEST SUPPORT OF THE 3RD GENERATION POWERHEAD, INCLUDING THE REFURBISHMENT OF THE FACET TEST RIG AND INTEGRATION OF THE POWERHEAD. THE CONTRACTOR SHALL PERFORM THE FOLLOWING TASKS: (1) TASK PLANNING AND STATUS REPORTS, (2) 3RD GENERATION COMBUSTOR OPTIMIZATION AND PRE-TEST ANALYSES, (3) FACET HARDWARE REFURBISHMENT, (4) 3RD GENERATION POWERHEAD FABRICATION AND RIG INTEGRATION (5) FACET HARDWARE INSTALLATION AND TEST SUPPORT, (6) POST-TEST DATA ANALYSIS AND REPORTING, AND (7) VEHICLE INTEGRATION ASSESSMENT. TASKS 1 AND 6 ARE REQUIRED TASKS AND TASK 7 HAS BEEN IDENTIFIED AS AN OPTIONAL TASK. THE CONTRACTOR SHALL ASSESS PERFORMANCE AND OPERABILITY THROUGH COMBUSTOR INLET INTERACTION AND POWERHEAD FLAME STABILITY AS IT RELATES TO THE FLIGHT RESEARCH VEHICLE CONCEPT DERIVED FROM THE STUDY CONDUCTED IN NASA CONTRACT: NNC10BA08B, TASK: NNC15TA03T. THE DERIVED FLIGHT RESEARCH VEHICLE DEFINITION AND ASSUMPTIONS WILL BE PROVIDED BY NASA. THE CONTRACTOR SHALL PROVIDE AN INTEGRATION ASSESSMENT OF THE DMRJ INTO THE VEHICLE AS A PART OF THE FINAL REPORT. THE CONTRACTOR SHALL PARTICIPATE AND PROVIDE SUPPORT IN THE DEVELOPMENT OF A NEXT STEPS CRITICAL GROUND DEMONSTRATION PLAN FOR REDUCING RISKS ASSOCIATED WITH TBCC PROPULSION TECHNOLOGIES. THIS PLAN WILL INCLUDE THE REUSABILITY CAPABILITY OF THE HARDWARE BEING EVALUATED FOR THIS CONTRACT, AS WELL AS ASSESSING A NEW INLET AND NOZZLE WHICH ARE SCALED VERSIONS OF THE FRV FROM NASA CONTRACT: NNC10BA08B, TASK: NNC15TA03T. THE CONTRACTOR SHALL DETERMINE THE CRITICAL ELEMENTS OF A COHESIVE PROPULSION GROUND DEMONSTRATION PROGRAM, DEFINE REQUIRED RISK REDUCTION GROUND TESTS, AND DEVELOP A BUDGETARY PLANNING ESTIMATE (BPE) AND INCLUDE/ADDRESS THESE ITEMS IN THE FINAL PRESENTATION. | AEROJET ROCKETDYNE OF DE, INC | $5,035,539 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR12SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; APPLIED RESEARCH | Mar 17, 2016 | Mar 17, 2016 | Aug 27, 2018 | ||
| IGF::OT::IGF BROAD AGENCY ANNOUNCEMENT TO AEROJET ROCKETDYNE FOR THE ADDITIVE MANUFACTURING QUALIFICATION PROCESS | AEROJET ROCKETDYNE OF DE, INC | $6,003,668 | DEPT OF THE AIR FORCE | DEPT OF THE AIR FORCE | — | 541712 | AC22NATIONAL DEFENSE R&D SERVICES; ATOMIC ENERGY DEFENSE ACTIVITIES; APPLIED RESEARCH | Dec 23, 2015 | Dec 23, 2015 | Mar 26, 2018 | ||
| IGF::CT::IGF RS-25 PRODUCTION RESTART TO BE UNDERTAKEN BY THE CONTRACTOR IN SUPPORT OF PROVIDING SIX RS-25 ENGINES MODIFIED AS NECESSARY FOR THE TECHNICAL REQUIREMENTS UNDER THE SPACE LAUNCH SYSTEM, RECERTIFICATION OF PRODUCTION, IMPROVEMENTS IN MANUFACTURING, AND CERTIFICATION FOR FLIGHT PROGRAM. | AEROJET ROCKETDYNE OF DE, INC | $3,923,125,643 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | 1675SPACE VEHICLE COMPONENTS | Nov 19, 2015 | Nov 1, 2015 | Sep 30, 2029 | ||
| IGF::OT::IGF CONTRACT AWARD FOR THE HIGH ALTITUDE VELOCITY (HAVOC) PROGRAM. | AEROJET ROCKETDYNE OF DE, INC | $320,284 | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541712 | AZ12 | Sep 15, 2015 | Sep 15, 2015 | Nov 16, 2016 | ||
| IGF::OT::IGF B TEST STAND COMMON CONTROL SYSTEM MODIFICATIONS | AEROJET ROCKETDYNE OF DE, INC | $350,414 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | C222ARCHITECT AND ENGINEERING- GENERAL: ELECTRICAL SYSTEMS | Jun 4, 2015 | Jun 4, 2015 | Mar 7, 2016 | ||
| IGF::OT::IGF DESIGN FABRICATION OF AN ULTRA-LOW COST ADDITIVE MANUFACTURED THRUST CHAMBER ASSEMBLY FOR A BANTAM ROCKET ENGINE POWERED | AEROJET ROCKETDYNE OF DE, INC | $467,018 | DEPT OF THE AIR FORCE | DEFENSE ADVANCED RESEARCH PROJECTS AGENCY (DARPA) | — | 541712 | AC62 | Sep 30, 2014 | Sep 30, 2014 | Mar 31, 2016 | ||
| IGF::OT::IGF DEVELOP AND DEMONSTRATE A POWER SYSTEM ARCHITECTURE FOR AN IN-SPACE TRANSPORTATION SEP-CENTRIC SPACECRAFT THAT MAXIMIZES THE ELECTRICAL AND THERMAL EFFICIENCIES OF THE POWERTRAIN BETWEEN THE SOLAR ARRAYS AND ELECTRIC PROPULSION THRUSTER TO REDUCE MASS, VOLUME AND COST TO THE SPACECRAFT WHILE ALSO TAKING INTO ACCOUNT THE REQUIREMENTS FOR THE OTHER SPACECRAFT SYSTEMS AND SUBSYSTEMS. | AEROJET ROCKETDYNE OF DE, INC | $0 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AZ11 | Sep 25, 2014 | Oct 1, 2014 | Mar 31, 2015 | ||
| IGF::CL::IGF MMRTG SUPPORT FOR THE MARS 2020 MISSION. | AEROJET ROCKETDYNE OF DE, INC | $7,917,742 | ENERGY, DEPARTMENT OF | ENERGY, DEPARTMENT OF | — | 541330Engineering Services | AR13SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; EXPERIMENTAL DEVELOPMENT | Jun 3, 2014 | Jun 2, 2014 | Aug 1, 2018 | ||
| CONTINUOUS DETONATION ENGINE RISK REDUCTION: LOW LOSS INLET/INJECTOR MANIFOLD | AEROJET ROCKETDYNE OF DE, INC | $879,303 | DEPT OF THE NAVY | DEPT OF THE NAVY | — | 541712 | AD92 | Apr 22, 2014 | Apr 22, 2014 | Jun 8, 2017 | ||
| IGF::OT::IGF NNC10BA13B/NNC13TA66T FOR ADDITIVE MANUFACTURING STUDY NASA AND THE UNITED STATES AIR FORCE (USAF) EMPLOY LAUNCH VEHICLES WITH UPPER STAGES THAT UTILIZE PRATT WHITNEY ROCKETDYNE (PWR) CORPORATION RL10 CLASS ENGINES. THE RL10 ENGINE IS RENOWNED IN THE HISTORY OF LIQUID ROCKET PROPULSION WITH VERSIONS POWERING LAUNCH VEHICLES FOR OVER 60 YEARS. WHILE CERTAIN ASPECTS AND TECHNOLOGIES USED IN THE RL10 CLASS ENGINES HAVE BEEN UPDATED, MANY OF THE PARTS ARE STILL HANDMADE WHICH SIGNIFICANTLY INCREASES THE PRODUCTION TIME AND COST OF THE FINISHED ENGINE BUILD. THE RL10 CLASS OF ENGINES IS CURRENTLY BASELINED FOR USAF AND NASA RELATED EXPENDABLE LAUNCH VEHICLES THROUGH 2030. WITH CURRENT FISCAL CHALLENGES FOR OUR COUNTRY, IT IS IMPERATIVE THAT THE RL10 PRODUCTION UNIT PRICE BE REDUCED. ONE OF THE BIGGEST CONTRIBUTORS TO ITS COST IS THE LARGE NUMBER OF TOUCH LABOR HOURS NECESSARY TO PRODUCE THIS ENGINE. THE PURPOSE OF THIS TASK IS TO INVESTIGATE THE APPLICABILITY OF AN ADVANCED MANUFACTURING METHOD REFERRED TO AS ADDITIVE MANUFACTURING TO REDUCE COMPONENT FABRICATION TIME, COST AND POTENTIALLY ENABLE PERFORMANCE IMPROVEMENTS. THE CONTRACTOR SHALL PERFORM TRADE STUDIES AND, IN CONJUNCTION WITH THE GOVERNMENT, SELECT HIGH PAYBACK PARTS OF THE RL10 ENGINE TO BE MANUFACTURED BY ADDITIVE MANUFACTURING PROCESS AND EXECUTE AN ENGINEERING AND VERIFICATION EFFORT TO CERTIFY THE SELECTED COMPONENTS ARE READY FOR PRODUCTION TRANSITION. THESE HIGH PAYBACK PARTS INCLUDE, BUT ARE NOT LIMITED TO: INJECTOR INTER PROPELLANT PLATE, IDDSI BRACKET, TURBOPUMP MOUNT BRACKETS, A-4-2 NOZZLE EXTENSION MOUNT BRACKETS, GIMBAL, MAIN FUEL SHUTOFF VALVE, ETC UNDER THE PROPOSED TASK ORDER NO. NNC13TA66T, PRATT AND WHITNEY ROCKETDYNE USING ADDITIVE MANUFACTURING TECHNIQUES SHALL DESIGN, DEVELOP, FABRICATE, TEST, VERIFY, AND CERTIFY SELECTED COMPONENTS SUCH THAT THEY MEET PERFORMANCE CRITERIA OF RL10 ENGINE SPECIFICATIONS. THE CONTRACTOR SHALL PERFORM PROGRAM MANAGEMENT, SYSTEMS ENGINEERING AND INTEGRATION, AND MANUFACTURING / PRODUCTION TRANSITION SUPPORT PLANNING. | AEROJET ROCKETDYNE OF DE, INC | $12,226,270 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541712 | AR13SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; EXPERIMENTAL DEVELOPMENT | Mar 11, 2014 | Mar 11, 2014 | Sep 24, 2016 | ||
| IGF::OT::IGF B2 TEST STAND ELECTRICAL BUILDOUT | AEROJET ROCKETDYNE OF DE, INC | $86,055 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541330Engineering Services | C222ARCHITECT AND ENGINEERING- GENERAL: ELECTRICAL SYSTEMS | Jan 8, 2014 | Jan 13, 2014 | Jan 12, 2015 | ||
| IGF:: OT IGF:: EW-201341, PRATT&WHITNEY ROCKETDYNE | AEROJET ROCKETDYNE OF DE, INC | $2,743,384 | DEPT OF THE ARMY | DEPT OF THE ARMY | — | 541712 | AH91 | Sep 25, 2013 | Sep 26, 2013 | Sep 24, 2019 | ||
| IGF::OT::IGF; BLANKET PURCHASE AGREEMENT CALL TASK ORDER (BTO) TO PROVIDE TECHNICAL SUPPORT (PHONE/E-MAIL/ON-SITE) FOR SETUP AND ACTIVATION OF THE DIGITAL DATA ACQUISITION SOFTWARE (DDAS) SOFTWARE AND MAINTENANCE OF THE SOFTWARE AS DEFINED IN THE STATEMENT OF WORK (SOW) AND THE BPA TERMS AND CONDITIONS FOR THE JOHN C. STENNIS SPACE CENTER (SSC), MS. THE PERIOD OF PERFORMANCE IS ONE YEAR FROM THE EFFECTIVE DATE OF THE BTO. | AEROJET ROCKETDYNE OF DE, INC | $22,061 | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | NATIONAL AERONAUTICS AND SPACE ADMINISTRATION | — | 541511Custom Computer Programming Services | D308 | Jun 27, 2013 | Jun 27, 2013 | Jun 26, 2014 |