Federal Contractor Profile
Aerojet Rocketdyne Of De, INC
$3.4B obligated·48 awards·3 agencies·10 NAICS
Federal Contracts
Showing contracts 151–196 of 196 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Apr 10, 2017 | Department of EnergyIDAHO OPERATIONS OFFICE | DENE0000687 | 541330 | IGF::CL::IGF MMRTG SUPPORT FOR THE MARS 2020 MISSION. | $1.3M |
| Mar 16, 2017 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM13AA33C | 336415 | IGF::OT::IGF SCIENCE MISSION STUDIES CONDUCTED BY THE ROBOTIC LUNAR LANDER (RLL) DEVELOPMENT PROJECT AT MSFC INDICATE THAT THE SPACECRAFT PROPULSION SYSTEM USED FOR THE MISSIONS MUST BE HIGH PERFORMANCE, LIGHTWEIGHT, AND COMPACT. HIGHLY MATURED TECHNOLOGY, LOW COST, AND SHORT DEVELOPMENT TIME ON THE PROPULSION SYSTEM ARE ALSO CRITICALLY DESIRABLE. SUBSEQUENTLY, THRUSTERS, BEING MAJOR PROPULSION COMPONENTS, HAVE BEEN IDENTIFIED AS HIGH RISK AND LONG-LEAD ITEMS FOR THE PROPULSION DEVELOPMENT. NASA MSFC FOR THE PAST SEVERAL YEARS HAS EVALUATED AVAILABLE OPERATIONAL MISSILE DEFENSE AGENCY (MDA) HERITAGE THRUSTERS SUITABLE FOR THE RLL PROPULSION SYSTEMS. HOT-FIRE TESTS OF 5-LBF AND 100-LBF THRUST-CLASS THRUSTERS DEMONSTRATED THAT THE MDA HERITAGE HARDWARE CAN BE IMPROVED TO MEET THE PROPULSION SYSTEM DEVELOPMENT OBJECTIVES: 1) LIGHTWEIGHT ON THRUSTER COMPONENTS AS WELL AS ON THE OVERALL SYSTEM; 2) LOW UNIT COST (IN COMPARISON WITH CONVENTIONAL THRUSTERS; 3) OPERATION OVER THE PROJECTED MISSION FLIGHT PROFILES, TOTAL BURN TIMES, AND ENTIRE MISSION DURATION; AND, 4) OPERATION WITH COLD PROPELLANTS (MON-25/MMH) FOR MINIMIZING THE HEATER POWER REQUIREMENT AND IN SPACE ENVIRONMENTS. FOR THIS NEXT YEAR NASA PLANS TO FOCUS ON THE MATURATION OF THE 100-LBF CLASS THRUSTER. STARTING FROM THE CURRENT TECHNOLOGY LEVEL, THE 100-LBF CLASS THRUSTER WILL BE EVOLVED THROUGH THE COMPLETION OF THE DESIGN VERIFICATION TEST PHASE. THE ENTIRE THRUSTER DEVELOPMENT IS EXPECTED TO COMPLETE WITHIN TWELVE MONTHS. THE REQUESTED EFFORT WILL BE DIVIDED INTO TWO WORK PERIODS (BASE AND OPTION PERIODS). THE BASE PERIOD IS PRIMARILY TO MAKE THE THRUSTER HARDWARE AND ASSOCIATED TEST SUPPORT COMPONENTS READY FOR HOT FIRE TESTS. THE WORK IN THIS PERIOD SHALL INCLUDE ALL HARDWARE DESIGN, FABRICATION, AND INTEGRATION OF THE TWO THRUSTER UNITS. THE DESIGN AND FABRICATION OF ALL HARDWARE TEST SUPPORT COMPONENTS SHALL BE ALSO PERFORMED. THE CONTRACTOR SHALL DESIGN THE THRUSTER TO MEET THE THRUSTER REQUIREMENTS SPECIFIED IN THE REFERENCED REQUIREMENTS DOCUMENT. THE CONTRACTOR SHALL DELIVER TWO INTEGRATED VALVE AND INJECTOR COMPONENTS AND PROVIDE ENGINEERING SUPPORT FOR COLD FLOW COMPONENT TESTING AT THE FACILITY SPECIFIED BY NASA. AFTER CONDUCTING THE COLD FLOW TESTING, THE VALVE AND INJECTOR COMPONENTS WOULD THEN BE RETURNED TO THE CONTRACTOR FOR THE FINAL THRUSTER ASSEMBLY. AT THE END OF THIS WORK PHASE. THE CONTRACTOR SHALL DELIVER TO NASA TWO ASSEMBLED THRUSTER UNITS, ALL ASSOCIATED INSTRUMENTATION AND TEST SETUP COMPONENTS READY FOR CONDUCTING DESIGN VERIFICATION TESTS. NASA WILL CHOOSE TO EXERCISE AN OPTION PERIOD BASED ON THE WORK PROGRESS OF THE BASE PERIOD AND FUNDING AVAILABILITY. THE OPTION PERIOD WILL EMPHASIZE ON THE DESIGN VERIFICATION HOT-FIRE TEST OF THE THRUSTER. TO ENSURE THE WORK IS ON SCHEDULE, THE OPTION PERIOD CAN BE PROPOSED TO START AT A TECHNICALLY-SOUNDED AND LOGICAL TIME DURING THE BASE PERIOD. THE CONTRACTOR SHALL PROVIDE THE FACILITY AND THE COORDINATION OF TESTING THE THRUSTERS IN VACUUM CONDITIONS WITH RLL MISSION RELEVANT COLD-TEMPERATURE PROPELLANTS. THE CONTRACTOR SHALL PROVIDE ALL NECESSARY ENGINEERING TEST SUPPORT, INCLUDING THE FORMULATION OF THE TEST PLAN, TO PERFORM THE THRUSTER TESTS. THE CONTRACTOR SHALL PROVIDE PROPELLANTS FOR THE TESTS. | $299K |
| Feb 27, 2017 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM13AA33C | 336415 | IGF::OT::IGF SCIENCE MISSION STUDIES CONDUCTED BY THE ROBOTIC LUNAR LANDER (RLL) DEVELOPMENT PROJECT AT MSFC INDICATE THAT THE SPACECRAFT PROPULSION SYSTEM USED FOR THE MISSIONS MUST BE HIGH PERFORMANCE, LIGHTWEIGHT, AND COMPACT. HIGHLY MATURED TECHNOLOGY, LOW COST, AND SHORT DEVELOPMENT TIME ON THE PROPULSION SYSTEM ARE ALSO CRITICALLY DESIRABLE. SUBSEQUENTLY, THRUSTERS, BEING MAJOR PROPULSION COMPONENTS, HAVE BEEN IDENTIFIED AS HIGH RISK AND LONG-LEAD ITEMS FOR THE PROPULSION DEVELOPMENT. NASA MSFC FOR THE PAST SEVERAL YEARS HAS EVALUATED AVAILABLE OPERATIONAL MISSILE DEFENSE AGENCY (MDA) HERITAGE THRUSTERS SUITABLE FOR THE RLL PROPULSION SYSTEMS. HOT-FIRE TESTS OF 5-LBF AND 100-LBF THRUST-CLASS THRUSTERS DEMONSTRATED THAT THE MDA HERITAGE HARDWARE CAN BE IMPROVED TO MEET THE PROPULSION SYSTEM DEVELOPMENT OBJECTIVES: 1) LIGHTWEIGHT ON THRUSTER COMPONENTS AS WELL AS ON THE OVERALL SYSTEM; 2) LOW UNIT COST (IN COMPARISON WITH CONVENTIONAL THRUSTERS; 3) OPERATION OVER THE PROJECTED MISSION FLIGHT PROFILES, TOTAL BURN TIMES, AND ENTIRE MISSION DURATION; AND, 4) OPERATION WITH COLD PROPELLANTS (MON-25/MMH) FOR MINIMIZING THE HEATER POWER REQUIREMENT AND IN SPACE ENVIRONMENTS. FOR THIS NEXT YEAR NASA PLANS TO FOCUS ON THE MATURATION OF THE 100-LBF CLASS THRUSTER. STARTING FROM THE CURRENT TECHNOLOGY LEVEL, THE 100-LBF CLASS THRUSTER WILL BE EVOLVED THROUGH THE COMPLETION OF THE DESIGN VERIFICATION TEST PHASE. THE ENTIRE THRUSTER DEVELOPMENT IS EXPECTED TO COMPLETE WITHIN TWELVE MONTHS. THE REQUESTED EFFORT WILL BE DIVIDED INTO TWO WORK PERIODS (BASE AND OPTION PERIODS). THE BASE PERIOD IS PRIMARILY TO MAKE THE THRUSTER HARDWARE AND ASSOCIATED TEST SUPPORT COMPONENTS READY FOR HOT FIRE TESTS. THE WORK IN THIS PERIOD SHALL INCLUDE ALL HARDWARE DESIGN, FABRICATION, AND INTEGRATION OF THE TWO THRUSTER UNITS. THE DESIGN AND FABRICATION OF ALL HARDWARE TEST SUPPORT COMPONENTS SHALL BE ALSO PERFORMED. THE CONTRACTOR SHALL DESIGN THE THRUSTER TO MEET THE THRUSTER REQUIREMENTS SPECIFIED IN THE REFERENCED REQUIREMENTS DOCUMENT. THE CONTRACTOR SHALL DELIVER TWO INTEGRATED VALVE AND INJECTOR COMPONENTS AND PROVIDE ENGINEERING SUPPORT FOR COLD FLOW COMPONENT TESTING AT THE FACILITY SPECIFIED BY NASA. AFTER CONDUCTING THE COLD FLOW TESTING, THE VALVE AND INJECTOR COMPONENTS WOULD THEN BE RETURNED TO THE CONTRACTOR FOR THE FINAL THRUSTER ASSEMBLY. AT THE END OF THIS WORK PHASE. THE CONTRACTOR SHALL DELIVER TO NASA TWO ASSEMBLED THRUSTER UNITS, ALL ASSOCIATED INSTRUMENTATION AND TEST SETUP COMPONENTS READY FOR CONDUCTING DESIGN VERIFICATION TESTS. NASA WILL CHOOSE TO EXERCISE AN OPTION PERIOD BASED ON THE WORK PROGRESS OF THE BASE PERIOD AND FUNDING AVAILABILITY. THE OPTION PERIOD WILL EMPHASIZE ON THE DESIGN VERIFICATION HOT-FIRE TEST OF THE THRUSTER. TO ENSURE THE WORK IS ON SCHEDULE, THE OPTION PERIOD CAN BE PROPOSED TO START AT A TECHNICALLY-SOUNDED AND LOGICAL TIME DURING THE BASE PERIOD. THE CONTRACTOR SHALL PROVIDE THE FACILITY AND THE COORDINATION OF TESTING THE THRUSTERS IN VACUUM CONDITIONS WITH RLL MISSION RELEVANT COLD-TEMPERATURE PROPELLANTS. THE CONTRACTOR SHALL PROVIDE ALL NECESSARY ENGINEERING TEST SUPPORT, INCLUDING THE FORMULATION OF THE TEST PLAN, TO PERFORM THE THRUSTER TESTS. THE CONTRACTOR SHALL PROVIDE PROPELLANTS FOR THE TESTS. | $50K |
| Feb 22, 2017 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $33M |
| Feb 17, 2017 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $9.0M |
| Feb 13, 2017 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16TA65T | 541712 | IGF::OT::IGF TASK ORDER NNC16TA65T FOR LOW ENRICHED URANIUM ENGINE AND COST ANALYSIS. | $350K |
| Dec 21, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $21M |
| Dec 21, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $9.8M |
| Nov 30, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $19M |
| Nov 30, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM13AA33C | 336415 | IGF::OT::IGF SCIENCE MISSION STUDIES CONDUCTED BY THE ROBOTIC LUNAR LANDER (RLL) DEVELOPMENT PROJECT AT MSFC INDICATE THAT THE SPACECRAFT PROPULSION SYSTEM USED FOR THE MISSIONS MUST BE HIGH PERFORMANCE, LIGHTWEIGHT, AND COMPACT. HIGHLY MATURED TECHNOLOGY, LOW COST, AND SHORT DEVELOPMENT TIME ON THE PROPULSION SYSTEM ARE ALSO CRITICALLY DESIRABLE. SUBSEQUENTLY, THRUSTERS, BEING MAJOR PROPULSION COMPONENTS, HAVE BEEN IDENTIFIED AS HIGH RISK AND LONG-LEAD ITEMS FOR THE PROPULSION DEVELOPMENT. NASA MSFC FOR THE PAST SEVERAL YEARS HAS EVALUATED AVAILABLE OPERATIONAL MISSILE DEFENSE AGENCY (MDA) HERITAGE THRUSTERS SUITABLE FOR THE RLL PROPULSION SYSTEMS. HOT-FIRE TESTS OF 5-LBF AND 100-LBF THRUST-CLASS THRUSTERS DEMONSTRATED THAT THE MDA HERITAGE HARDWARE CAN BE IMPROVED TO MEET THE PROPULSION SYSTEM DEVELOPMENT OBJECTIVES: 1) LIGHTWEIGHT ON THRUSTER COMPONENTS AS WELL AS ON THE OVERALL SYSTEM; 2) LOW UNIT COST (IN COMPARISON WITH CONVENTIONAL THRUSTERS; 3) OPERATION OVER THE PROJECTED MISSION FLIGHT PROFILES, TOTAL BURN TIMES, AND ENTIRE MISSION DURATION; AND, 4) OPERATION WITH COLD PROPELLANTS (MON-25/MMH) FOR MINIMIZING THE HEATER POWER REQUIREMENT AND IN SPACE ENVIRONMENTS. FOR THIS NEXT YEAR NASA PLANS TO FOCUS ON THE MATURATION OF THE 100-LBF CLASS THRUSTER. STARTING FROM THE CURRENT TECHNOLOGY LEVEL, THE 100-LBF CLASS THRUSTER WILL BE EVOLVED THROUGH THE COMPLETION OF THE DESIGN VERIFICATION TEST PHASE. THE ENTIRE THRUSTER DEVELOPMENT IS EXPECTED TO COMPLETE WITHIN TWELVE MONTHS. THE REQUESTED EFFORT WILL BE DIVIDED INTO TWO WORK PERIODS (BASE AND OPTION PERIODS). THE BASE PERIOD IS PRIMARILY TO MAKE THE THRUSTER HARDWARE AND ASSOCIATED TEST SUPPORT COMPONENTS READY FOR HOT FIRE TESTS. THE WORK IN THIS PERIOD SHALL INCLUDE ALL HARDWARE DESIGN, FABRICATION, AND INTEGRATION OF THE TWO THRUSTER UNITS. THE DESIGN AND FABRICATION OF ALL HARDWARE TEST SUPPORT COMPONENTS SHALL BE ALSO PERFORMED. THE CONTRACTOR SHALL DESIGN THE THRUSTER TO MEET THE THRUSTER REQUIREMENTS SPECIFIED IN THE REFERENCED REQUIREMENTS DOCUMENT. THE CONTRACTOR SHALL DELIVER TWO INTEGRATED VALVE AND INJECTOR COMPONENTS AND PROVIDE ENGINEERING SUPPORT FOR COLD FLOW COMPONENT TESTING AT THE FACILITY SPECIFIED BY NASA. AFTER CONDUCTING THE COLD FLOW TESTING, THE VALVE AND INJECTOR COMPONENTS WOULD THEN BE RETURNED TO THE CONTRACTOR FOR THE FINAL THRUSTER ASSEMBLY. AT THE END OF THIS WORK PHASE. THE CONTRACTOR SHALL DELIVER TO NASA TWO ASSEMBLED THRUSTER UNITS, ALL ASSOCIATED INSTRUMENTATION AND TEST SETUP COMPONENTS READY FOR CONDUCTING DESIGN VERIFICATION TESTS. NASA WILL CHOOSE TO EXERCISE AN OPTION PERIOD BASED ON THE WORK PROGRESS OF THE BASE PERIOD AND FUNDING AVAILABILITY. THE OPTION PERIOD WILL EMPHASIZE ON THE DESIGN VERIFICATION HOT-FIRE TEST OF THE THRUSTER. TO ENSURE THE WORK IS ON SCHEDULE, THE OPTION PERIOD CAN BE PROPOSED TO START AT A TECHNICALLY-SOUNDED AND LOGICAL TIME DURING THE BASE PERIOD. THE CONTRACTOR SHALL PROVIDE THE FACILITY AND THE COORDINATION OF TESTING THE THRUSTERS IN VACUUM CONDITIONS WITH RLL MISSION RELEVANT COLD-TEMPERATURE PROPELLANTS. THE CONTRACTOR SHALL PROVIDE ALL NECESSARY ENGINEERING TEST SUPPORT, INCLUDING THE FORMULATION OF THE TEST PLAN, TO PERFORM THE THRUSTER TESTS. THE CONTRACTOR SHALL PROVIDE PROPELLANTS FOR THE TESTS. | $52K |
| Nov 29, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $6.0M |
| Oct 28, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $7.0M |
| Oct 20, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $13M |
| Sep 28, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $6.0M |
| Sep 28, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $17M |
| Sep 15, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $550K |
| Aug 29, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16TA03T | 541712 | 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. | $33K |
| Aug 15, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $12M |
| Aug 15, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $1.5M |
| Aug 10, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $5.6M |
| Aug 9, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $20M |
| Aug 5, 2016 | National Aeronautics and Space AdministrationNASA GLENN RESEARCH CENTER | NNC16TA65T | 541712 | IGF::OT::IGF TASK ORDER NNC16TA65T FOR LOW ENRICHED URANIUM ENGINE AND COST ANALYSIS. | $500K |
| Jul 7, 2016 | National Aeronautics and Space AdministrationNASA STENNIS SPACE CENTER | NNS16AA05P | 541330 | IGF::OT::IGF: B TEST STAND LH&LOX DOCK CONTROL PANELS | $274K |
| Jun 14, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $10M |
| May 18, 2016 | Department of EnergyIDAHO OPERATIONS OFFICE | DENE0000687 | 541330 | IGF::CL::IGF MMRTG SUPPORT FOR THE MARS 2020 MISSION. | $1.5M |
| Apr 27, 2016 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865016C7633 | 541712 | IGF::OT::IGF GRIFFIN | $595K |
| Apr 22, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $8.0M |
| Apr 13, 2016 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $32M |
| Mar 17, 2016 | National Aeronautics and Space AdministrationGLENN RESEARCH CENTER | NNC16TA03T | 541712 | 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. | $4.5M |
| Feb 25, 2016 | Department of EnergyIDAHO OPERATIONS OFFICE | DENE0000687 | 541330 | IGF::CL::IGF MMRTG SUPPORT FOR THE MARS 2020 MISSION. | $380K |
| Feb 10, 2016 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $53M |
| Jan 27, 2016 | National Aeronautics and Space AdministrationGLENN RESEARCH CENTER | NNC15BA09B | 541712 | IGF::OT::IGF TO SUPPORT THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION'S LONG STANDING OBJECTIVE TO DEVELOP, DEMONSTRATE, AND VERIFY ADVANCED PROPULSION SYSTEM TECHNOLOGIES,CONTRACT NNC15BA05B RESEARCH AND TECHNOLOGIES FOR AEROSPACE PROPULSION SYSTEMS 2 - RTAPS 2 - TECHNOLOGY AREA 2 FOR: SOW TECHNOLOGY AREA 2: SPACE PROPULSION THAT CONSISTS OF SIX (6) ELEMENTS: ELEMENT 2.2.1 PROPULSION SYSTEM DESIGN AND TRADE STUDIES ELEMENT 2.2.2 LIQUID ENGINE SYSTEMS ELEMENT 2.2.3 PROPELLANT SYSTEMS ELEMENT 2.2.4 ELECTRIC PROPULSION ELEMENT 2.2.5 ROCKET-BASED, COMBINED CYCLE PROPULSION SYSTEMS ELEMENT 2.2.6 ADVANCED PROPULSION SYSTEMS IGF::OF::IGF | $30K |
| Jan 25, 2016 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $30M |
| Jan 22, 2016 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $10M |
| Jan 21, 2016 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM13AA33C | 336415 | IGF::OT::IGF SCIENCE MISSION STUDIES CONDUCTED BY THE ROBOTIC LUNAR LANDER (RLL) DEVELOPMENT PROJECT AT MSFC INDICATE THAT THE SPACECRAFT PROPULSION SYSTEM USED FOR THE MISSIONS MUST BE HIGH PERFORMANCE, LIGHTWEIGHT, AND COMPACT. HIGHLY MATURED TECHNOLOGY, LOW COST, AND SHORT DEVELOPMENT TIME ON THE PROPULSION SYSTEM ARE ALSO CRITICALLY DESIRABLE. SUBSEQUENTLY, THRUSTERS, BEING MAJOR PROPULSION COMPONENTS, HAVE BEEN IDENTIFIED AS HIGH RISK AND LONG-LEAD ITEMS FOR THE PROPULSION DEVELOPMENT. NASA MSFC FOR THE PAST SEVERAL YEARS HAS EVALUATED AVAILABLE OPERATIONAL MISSILE DEFENSE AGENCY (MDA) HERITAGE THRUSTERS SUITABLE FOR THE RLL PROPULSION SYSTEMS. HOT-FIRE TESTS OF 5-LBF AND 100-LBF THRUST-CLASS THRUSTERS DEMONSTRATED THAT THE MDA HERITAGE HARDWARE CAN BE IMPROVED TO MEET THE PROPULSION SYSTEM DEVELOPMENT OBJECTIVES: 1) LIGHTWEIGHT ON THRUSTER COMPONENTS AS WELL AS ON THE OVERALL SYSTEM; 2) LOW UNIT COST (IN COMPARISON WITH CONVENTIONAL THRUSTERS; 3) OPERATION OVER THE PROJECTED MISSION FLIGHT PROFILES, TOTAL BURN TIMES, AND ENTIRE MISSION DURATION; AND, 4) OPERATION WITH COLD PROPELLANTS (MON-25/MMH) FOR MINIMIZING THE HEATER POWER REQUIREMENT AND IN SPACE ENVIRONMENTS. FOR THIS NEXT YEAR NASA PLANS TO FOCUS ON THE MATURATION OF THE 100-LBF CLASS THRUSTER. STARTING FROM THE CURRENT TECHNOLOGY LEVEL, THE 100-LBF CLASS THRUSTER WILL BE EVOLVED THROUGH THE COMPLETION OF THE DESIGN VERIFICATION TEST PHASE. THE ENTIRE THRUSTER DEVELOPMENT IS EXPECTED TO COMPLETE WITHIN TWELVE MONTHS. THE REQUESTED EFFORT WILL BE DIVIDED INTO TWO WORK PERIODS (BASE AND OPTION PERIODS). THE BASE PERIOD IS PRIMARILY TO MAKE THE THRUSTER HARDWARE AND ASSOCIATED TEST SUPPORT COMPONENTS READY FOR HOT FIRE TESTS. THE WORK IN THIS PERIOD SHALL INCLUDE ALL HARDWARE DESIGN, FABRICATION, AND INTEGRATION OF THE TWO THRUSTER UNITS. THE DESIGN AND FABRICATION OF ALL HARDWARE TEST SUPPORT COMPONENTS SHALL BE ALSO PERFORMED. THE CONTRACTOR SHALL DESIGN THE THRUSTER TO MEET THE THRUSTER REQUIREMENTS SPECIFIED IN THE REFERENCED REQUIREMENTS DOCUMENT. THE CONTRACTOR SHALL DELIVER TWO INTEGRATED VALVE AND INJECTOR COMPONENTS AND PROVIDE ENGINEERING SUPPORT FOR COLD FLOW COMPONENT TESTING AT THE FACILITY SPECIFIED BY NASA. AFTER CONDUCTING THE COLD FLOW TESTING, THE VALVE AND INJECTOR COMPONENTS WOULD THEN BE RETURNED TO THE CONTRACTOR FOR THE FINAL THRUSTER ASSEMBLY. AT THE END OF THIS WORK PHASE. THE CONTRACTOR SHALL DELIVER TO NASA TWO ASSEMBLED THRUSTER UNITS, ALL ASSOCIATED INSTRUMENTATION AND TEST SETUP COMPONENTS READY FOR CONDUCTING DESIGN VERIFICATION TESTS. NASA WILL CHOOSE TO EXERCISE AN OPTION PERIOD BASED ON THE WORK PROGRESS OF THE BASE PERIOD AND FUNDING AVAILABILITY. THE OPTION PERIOD WILL EMPHASIZE ON THE DESIGN VERIFICATION HOT-FIRE TEST OF THE THRUSTER. TO ENSURE THE WORK IS ON SCHEDULE, THE OPTION PERIOD CAN BE PROPOSED TO START AT A TECHNICALLY-SOUNDED AND LOGICAL TIME DURING THE BASE PERIOD. THE CONTRACTOR SHALL PROVIDE THE FACILITY AND THE COORDINATION OF TESTING THE THRUSTERS IN VACUUM CONDITIONS WITH RLL MISSION RELEVANT COLD-TEMPERATURE PROPELLANTS. THE CONTRACTOR SHALL PROVIDE ALL NECESSARY ENGINEERING TEST SUPPORT, INCLUDING THE FORMULATION OF THE TEST PLAN, TO PERFORM THE THRUSTER TESTS. THE CONTRACTOR SHALL PROVIDE PROPELLANTS FOR THE TESTS. | $86K |
| Jan 20, 2016 | National Aeronautics and Space AdministrationSTENNIS SPACE CENTER | SSC00200201DNAS1302014 | 541380 | HARDWARE ASSURANCE PROPULSION TESTING, TEST SUPPORT SERVICES OF SPACE SHUTTLE MAIN ENGINE SSME | $40K |
| Dec 24, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $3.6M |
| Dec 23, 2015 | Department of DefenseFA8814 SPACE DEV TEST PLAN PKT LA | FA881416C0002 | 541712 | IGF::OT::IGF BROAD AGENCY ANNOUNCEMENT TO AEROJET ROCKETDYNE FOR THE ADDITIVE MANUFACTURING QUALIFICATION PROCESS | $6.0M |
| Dec 23, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $10M |
| Dec 18, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM13AA33C | 336415 | IGF::OT::IGF SCIENCE MISSION STUDIES CONDUCTED BY THE ROBOTIC LUNAR LANDER (RLL) DEVELOPMENT PROJECT AT MSFC INDICATE THAT THE SPACECRAFT PROPULSION SYSTEM USED FOR THE MISSIONS MUST BE HIGH PERFORMANCE, LIGHTWEIGHT, AND COMPACT. HIGHLY MATURED TECHNOLOGY, LOW COST, AND SHORT DEVELOPMENT TIME ON THE PROPULSION SYSTEM ARE ALSO CRITICALLY DESIRABLE. SUBSEQUENTLY, THRUSTERS, BEING MAJOR PROPULSION COMPONENTS, HAVE BEEN IDENTIFIED AS HIGH RISK AND LONG-LEAD ITEMS FOR THE PROPULSION DEVELOPMENT. NASA MSFC FOR THE PAST SEVERAL YEARS HAS EVALUATED AVAILABLE OPERATIONAL MISSILE DEFENSE AGENCY (MDA) HERITAGE THRUSTERS SUITABLE FOR THE RLL PROPULSION SYSTEMS. HOT-FIRE TESTS OF 5-LBF AND 100-LBF THRUST-CLASS THRUSTERS DEMONSTRATED THAT THE MDA HERITAGE HARDWARE CAN BE IMPROVED TO MEET THE PROPULSION SYSTEM DEVELOPMENT OBJECTIVES: 1) LIGHTWEIGHT ON THRUSTER COMPONENTS AS WELL AS ON THE OVERALL SYSTEM; 2) LOW UNIT COST (IN COMPARISON WITH CONVENTIONAL THRUSTERS; 3) OPERATION OVER THE PROJECTED MISSION FLIGHT PROFILES, TOTAL BURN TIMES, AND ENTIRE MISSION DURATION; AND, 4) OPERATION WITH COLD PROPELLANTS (MON-25/MMH) FOR MINIMIZING THE HEATER POWER REQUIREMENT AND IN SPACE ENVIRONMENTS. FOR THIS NEXT YEAR NASA PLANS TO FOCUS ON THE MATURATION OF THE 100-LBF CLASS THRUSTER. STARTING FROM THE CURRENT TECHNOLOGY LEVEL, THE 100-LBF CLASS THRUSTER WILL BE EVOLVED THROUGH THE COMPLETION OF THE DESIGN VERIFICATION TEST PHASE. THE ENTIRE THRUSTER DEVELOPMENT IS EXPECTED TO COMPLETE WITHIN TWELVE MONTHS. THE REQUESTED EFFORT WILL BE DIVIDED INTO TWO WORK PERIODS (BASE AND OPTION PERIODS). THE BASE PERIOD IS PRIMARILY TO MAKE THE THRUSTER HARDWARE AND ASSOCIATED TEST SUPPORT COMPONENTS READY FOR HOT FIRE TESTS. THE WORK IN THIS PERIOD SHALL INCLUDE ALL HARDWARE DESIGN, FABRICATION, AND INTEGRATION OF THE TWO THRUSTER UNITS. THE DESIGN AND FABRICATION OF ALL HARDWARE TEST SUPPORT COMPONENTS SHALL BE ALSO PERFORMED. THE CONTRACTOR SHALL DESIGN THE THRUSTER TO MEET THE THRUSTER REQUIREMENTS SPECIFIED IN THE REFERENCED REQUIREMENTS DOCUMENT. THE CONTRACTOR SHALL DELIVER TWO INTEGRATED VALVE AND INJECTOR COMPONENTS AND PROVIDE ENGINEERING SUPPORT FOR COLD FLOW COMPONENT TESTING AT THE FACILITY SPECIFIED BY NASA. AFTER CONDUCTING THE COLD FLOW TESTING, THE VALVE AND INJECTOR COMPONENTS WOULD THEN BE RETURNED TO THE CONTRACTOR FOR THE FINAL THRUSTER ASSEMBLY. AT THE END OF THIS WORK PHASE. THE CONTRACTOR SHALL DELIVER TO NASA TWO ASSEMBLED THRUSTER UNITS, ALL ASSOCIATED INSTRUMENTATION AND TEST SETUP COMPONENTS READY FOR CONDUCTING DESIGN VERIFICATION TESTS. NASA WILL CHOOSE TO EXERCISE AN OPTION PERIOD BASED ON THE WORK PROGRESS OF THE BASE PERIOD AND FUNDING AVAILABILITY. THE OPTION PERIOD WILL EMPHASIZE ON THE DESIGN VERIFICATION HOT-FIRE TEST OF THE THRUSTER. TO ENSURE THE WORK IS ON SCHEDULE, THE OPTION PERIOD CAN BE PROPOSED TO START AT A TECHNICALLY-SOUNDED AND LOGICAL TIME DURING THE BASE PERIOD. THE CONTRACTOR SHALL PROVIDE THE FACILITY AND THE COORDINATION OF TESTING THE THRUSTERS IN VACUUM CONDITIONS WITH RLL MISSION RELEVANT COLD-TEMPERATURE PROPELLANTS. THE CONTRACTOR SHALL PROVIDE ALL NECESSARY ENGINEERING TEST SUPPORT, INCLUDING THE FORMULATION OF THE TEST PLAN, TO PERFORM THE THRUSTER TESTS. THE CONTRACTOR SHALL PROVIDE PROPELLANTS FOR THE TESTS. | $124K |
| Dec 8, 2015 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001414C0035 | 541712 | CONTINUOUS DETONATION ENGINE RISK REDUCTION: LOW LOSS INLET/INJECTOR MANIFOLD | $100K |
| Dec 1, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $10M |
| Nov 30, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $7.0M |
| Nov 19, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM16AA02C | 541712 | 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. | $3.1M |
| Nov 13, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $6.5M |
| Oct 27, 2015 | National Aeronautics and Space AdministrationMARSHALL SPACE FLIGHT CENTER | NNM06AB13C | 541710 | LETTER CONTRACT TO INITIATE DDT&E AND LONG LEAD PURCHASES | $9.1M |
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