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Department of Defense
This contract includes 1 purchase order from Apr 21, 2021 to Apr 21, 2021
| Buyer | Vendor | Issued Date | Quantity |
|---|---|---|---|
| Department of Defense | Bowhead Base Operations LLC | Apr 21, 2021 | 1 |
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NASA Goddard Space Flight Center
IGF::OT::IGF THIS CONTRACT IS FOR IBEX INTERSTELLAR BOUNDARY EXPLORER (IBEX) SUPPORT. THIS CONTRACT IS A RESULT OF A PI TRANSFER FROM NNG05EC85C. THE CONTRACTOR SHALL BE RESPONSIBLE FOR THE CONDUCT OF ALL PHASES AND ASPECTS OF THE IBEX MISSION INCLUDING: 1) LIFE-CYCLE PROJECT MANAGEMENT 2) DESIGN, TEST, DEVELOPMENT, AND OPERATIONS (PAYLOAD, SPACECRAFT, LAUNCH VEHICLE, SPACECRAFT TO LAUNCH-VEHICLE INTERFACES, LAUNCH AND FLIGHT OPERATIONS) AND 3) POST-OPERATIONS DATA ANALYSIS AND ARCHIVING. IN PERFORMANCE OF THIS EFFORT, THE IBEX TEAM SHALL: A. MANAGE THE PROJECT, PROVIDE COST AND SCHEDULE INFORMATION TO NASA AS SPECIFIED IN 3.0 MANAGEMENT, ABOVE. B. PROVIDE DAY-TO-DAY MANAGEMENT AND COORDINATION OF THE PROJECT AS DELEGATED BY THE PI TO THE PROJECT MANAGER (PM), INCLUDING MONITORING AND REPORTING TECHNICAL PROGRESS AND FINANCIAL STATUS, IMPLEMENTING THE RISK MANAGEMENT PLAN AND CONDUCTING MISSION LEVEL REVIEWS AS SPECIFIED IN SECTION 4.3, SYSTEM LEVEL REVIEWS. C. CONDUCT REVIEWS FOR ALL PAYLOAD SENSORS, PAYLOAD SUPPORT INFRASTRUCTURE AND ASSOCIATED GSE. D. PERFORM SCIENTIFIC ANALYSES IN SUPPORT OF THE MISSION SCIENCE REQUIREMENTS. E. PERFORM SYSTEMS ENGINEERING TO COORDINATE THE DESIGN OF THE INSTRUMENT COMPLEMENT AND SPACECRAFT BUS COMPONENTS AND TO ENSURE THE COMPATIBILITY OF THE SPACE-TO-GROUND AND NETWORK COMMUNICATIONS. F. PERFORM TRADE STUDIES TO ELIMINATE AND MITIGATE RISKS G. DELIVER THE IBEX FLIGHT SEGMENT TO VANDENBERG AIR FORCE BASE (VAFB), SUPPORT INTEGRATION WITH THE LAUNCH VEHICLE, AND ASSIST THE LAUNCH OPERATIONS H. ESTABLISH THE MISSION CONTROL CENTER (MCC) AND IBEX SCIENCE OPERATIONS AND DATA ANALYSIS CENTER (ISOC) INCLUDING ALL COMPUTERS, NETWORKS, AND OPERATING SOFTWARE, INSTRUMENT DATABASES AND PROCEDURES NECESSARY TO FUNCTIONALLY TEST AND LATER CONTROL THE SPACECRAFT I. HOLD SCIENCE TEAM MEETINGS AS WELL AS TECHNICAL INTERCHANGE MEETINGS. J. BASELINE THE SCIENCE REQUIREMENTS AND SCIENCE ANALYSIS PLAN INTO AN IBEX MISSION DEFINITION REQUIREMENTS AGREEMENT (MDRA) AND THE IBEX DATA MANAGEMENT PLAN. K. IMPLEMENT AN APPROVED MISSION ASSURANCE PLAN. L. IMPLEMENT A SYSTEMS ENGINEERING FUNCTION TO VERIFY PERFORMANCE SPECIFICATION COMPLIANCE TO THE MISSION SCIENCE REQUIREMENTS. M. DESIGN, FABRICATE, INTEGRATE AND TEST THE PAYLOAD, SPACECRAFT, SOLID ROCKET MOTOR AND LAUNCH VEHICLE ADAPTER, AND INTEGRATE THE IBEX FLIGHT SEGMENT WITH THE LAUNCH VEHICLE. N. IMPLEMENT A SAFETY PROGRAM INCLUDING THE GENERATION OF THE MISSILE SYSTEM PRE-LAUNCH SAFETY PACKAGE (MSPSP). O. SUPPORT LAUNCH, PERFORM ON-ORBIT CHECKOUT, AND ESTABLISH ON-ORBIT DATA ACQUISITION CONTACT WITH THE PAYLOAD. WITHIN THE FIRST 30 DAYS AFTER LAUNCH, INITIAL ENGINEERING AND SCIENCE CHECKOUT AND VERIFICATION OF SPACECRAFT IN-FLIGHT OPERATION WILL BE PERFORMED. P. PROVIDE THE SERVICES OF THE MCC AND THE ISOC. Q. CONDUCT THE E/PO PROGRAM IN COOPERATION WITH THE IDENTIFIED TEAM MEMBERS.
Effective Date
Mar 23, 2017
Expires
Effective: Mar 23, 2017
NASA Goddard Space Flight Center
Expires:
IGF::OT::IGF THIS CONTRACT IS FOR IBEX INTERSTELLAR BOUNDARY EXPLORER (IBEX) SUPPORT. THIS CONTRACT IS A RESULT OF A PI TRANSFER FROM NNG05EC85C. THE CONTRACTOR SHALL BE RESPONSIBLE FOR THE CONDUCT OF ALL PHASES AND ASPECTS OF THE IBEX MISSION INCLUDING: 1) LIFE-CYCLE PROJECT MANAGEMENT 2) DESIGN, TEST, DEVELOPMENT, AND OPERATIONS (PAYLOAD, SPACECRAFT, LAUNCH VEHICLE, SPACECRAFT TO LAUNCH-VEHICLE INTERFACES, LAUNCH AND FLIGHT OPERATIONS) AND 3) POST-OPERATIONS DATA ANALYSIS AND ARCHIVING. IN PERFORMANCE OF THIS EFFORT, THE IBEX TEAM SHALL: A. MANAGE THE PROJECT, PROVIDE COST AND SCHEDULE INFORMATION TO NASA AS SPECIFIED IN 3.0 MANAGEMENT, ABOVE. B. PROVIDE DAY-TO-DAY MANAGEMENT AND COORDINATION OF THE PROJECT AS DELEGATED BY THE PI TO THE PROJECT MANAGER (PM), INCLUDING MONITORING AND REPORTING TECHNICAL PROGRESS AND FINANCIAL STATUS, IMPLEMENTING THE RISK MANAGEMENT PLAN AND CONDUCTING MISSION LEVEL REVIEWS AS SPECIFIED IN SECTION 4.3, SYSTEM LEVEL REVIEWS. C. CONDUCT REVIEWS FOR ALL PAYLOAD SENSORS, PAYLOAD SUPPORT INFRASTRUCTURE AND ASSOCIATED GSE. D. PERFORM SCIENTIFIC ANALYSES IN SUPPORT OF THE MISSION SCIENCE REQUIREMENTS. E. PERFORM SYSTEMS ENGINEERING TO COORDINATE THE DESIGN OF THE INSTRUMENT COMPLEMENT AND SPACECRAFT BUS COMPONENTS AND TO ENSURE THE COMPATIBILITY OF THE SPACE-TO-GROUND AND NETWORK COMMUNICATIONS. F. PERFORM TRADE STUDIES TO ELIMINATE AND MITIGATE RISKS G. DELIVER THE IBEX FLIGHT SEGMENT TO VANDENBERG AIR FORCE BASE (VAFB), SUPPORT INTEGRATION WITH THE LAUNCH VEHICLE, AND ASSIST THE LAUNCH OPERATIONS H. ESTABLISH THE MISSION CONTROL CENTER (MCC) AND IBEX SCIENCE OPERATIONS AND DATA ANALYSIS CENTER (ISOC) INCLUDING ALL COMPUTERS, NETWORKS, AND OPERATING SOFTWARE, INSTRUMENT DATABASES AND PROCEDURES NECESSARY TO FUNCTIONALLY TEST AND LATER CONTROL THE SPACECRAFT I. HOLD SCIENCE TEAM MEETINGS AS WELL AS TECHNICAL INTERCHANGE MEETINGS. J. BASELINE THE SCIENCE REQUIREMENTS AND SCIENCE ANALYSIS PLAN INTO AN IBEX MISSION DEFINITION REQUIREMENTS AGREEMENT (MDRA) AND THE IBEX DATA MANAGEMENT PLAN. K. IMPLEMENT AN APPROVED MISSION ASSURANCE PLAN. L. IMPLEMENT A SYSTEMS ENGINEERING FUNCTION TO VERIFY PERFORMANCE SPECIFICATION COMPLIANCE TO THE MISSION SCIENCE REQUIREMENTS. M. DESIGN, FABRICATE, INTEGRATE AND TEST THE PAYLOAD, SPACECRAFT, SOLID ROCKET MOTOR AND LAUNCH VEHICLE ADAPTER, AND INTEGRATE THE IBEX FLIGHT SEGMENT WITH THE LAUNCH VEHICLE. N. IMPLEMENT A SAFETY PROGRAM INCLUDING THE GENERATION OF THE MISSILE SYSTEM PRE-LAUNCH SAFETY PACKAGE (MSPSP). O. SUPPORT LAUNCH, PERFORM ON-ORBIT CHECKOUT, AND ESTABLISH ON-ORBIT DATA ACQUISITION CONTACT WITH THE PAYLOAD. WITHIN THE FIRST 30 DAYS AFTER LAUNCH, INITIAL ENGINEERING AND SCIENCE CHECKOUT AND VERIFICATION OF SPACECRAFT IN-FLIGHT OPERATION WILL BE PERFORMED. P. PROVIDE THE SERVICES OF THE MCC AND THE ISOC. Q. CONDUCT THE E/PO PROGRAM IN COOPERATION WITH THE IDENTIFIED TEAM MEMBERS.
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NASA Marshall Space Flight Center
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.
Effective Date
Sep 1, 2007
Expires
Effective: Sep 1, 2007
NASA Marshall Space Flight Center
Expires:
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.
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