Order to BOWHEAD PROGRAM MANAGEMENT & OPERATIONS, LLC by Department of the Navy for NON-PERSONAL ENGINEERING, TECHNICAL, LOGISTICS, CONFIGURATION MANAGEMENT, DATA MANAGEMENT, AND PROGRAM MANAGEMENT SUPPORT SERVICES FOR THE NSWC CRANE STRATEGIC SYSTEMS GUIDANCE, NAVIGATION AND CONTROL DIVISION, CODE GXP.

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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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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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IGF::OT::IGF NEXTSTEP NRA AWARD. THIS NEXTSTEP CONTRACT BUILDS UPON THE SUCCESS OF COMMERCIAL ORBITAL TRANSPORTATION SERVICES SPACE ACT AGREEMENT DEVELOPMENT PROGRAM AND AN EXISTING INTERNATIONAL SPACE STATION (ISS) COMMERCIAL RESUPPLY SERVICES (CRS) CONTRACT. ORBITAL HAS SUCCESSFULLY TRANSITIONED FROM COTS TO THE CRS PROGRAM, FLYING THREE VERY SUCCESSFUL PRESSURIZED CARGO RESUPPLY MISSIONS TO THE ISS, USING THE CYGNUS SPACECRAFT. ORBITAL ALSO SUCCESSFULLY DEVELOPED SPACECRAFT FOR SOLAR SYSTEM EXPLORATION TO INCLUDE THE CURRENTLY OPERATIONAL DAWN MISSION. THIS MISSION WAS LAUNCHED IN SEPTEMBER 2007, COMPLETED ITS RENDEZVOUS MISSION AT VESTA IN JULY 2012 AND IS EN ROUTE TO CERES IN EARLY 2015. WITH SPACE AGENCY BUDGETS CONTINUING TO BE TIGHT, EXPLORATION PLANS NEED TO EMPHASIZE EVOLUTION OF EXISTING SYSTEMS, WHERE COST AND SCHEDULE IS BETTER CONTROLLED, AND DEVELOPMENT RISK REDUCED. SPECIFICALLY, ELEMENTS OF THE CURRENT ISS, INCLUDING CYGNUS, CAN BE EVOLVED TO SUPPORT MORE DISTANT SPACE DESTINATIONS. TO SUPPORT THESE ENDEAVORS, ORBITAL CONTRIBUTES TO THE DEVELOPMENT AND PRODUCT IMPROVEMENT OF CYGNUS AND TO NEXTSTEP ACTIVITIES AND HAVE INVESTED IN THE COTS CRS PUBLIC-PRIVATE PARTNERSHIP ENDEAVOR. ORBITAL'S EXPLORATION AUGMENTATION MODULE (BAM) ARCHITECTURE USES A MODULAR, BUILDING BLOCK APPROACH THAT LEVERAGES THE CYGNUS SPACECRAFT TO EXPAND CISLUNAR AND LONG DURATION DEEP SPACE TRANSIT HABITATION CAPABILITIES AND TECHNOLOGIES CRITICAL TO NASAS LONG-TERM EXPLORATION GOALS. ORBITALS ARCHITECTURE CONCEPT BLENDS IN-PRODUCTION HARDWARE WITH ADAPTATION, EVOLUTION, PLANNING, AND FORWARD THINKING. CYGNUS WILL SERVE AS A MODULAR HABITAT AND TEST PLATFORM FOR QUALIFYING TECHNOLOGIES IN A DISTANT RETROGRADE ORBIT (DRO) OR IN A LOW EARTH ORBIT (LEO), EITHER WHILE ATTACHED TO THE ISS OR AS A FREE-FLYER. USING THE EXISTING, OPERATIONAL CYGNUS TO PERFORM THESE MISSIONS HAS THE ADVANTAGE OF DECREASING OVERALL DEVELOPMENT TIME AND COSTS, AND FREEING UP RESOURCES THAT WOULD BE SPENT ON DEVELOPING A SPACECRAFT TO FOCUS ON CULTIVATING MISSION ENABLING TECHNOLOGIES. THE GOAL IS TO HAVE A CYGNUS DERIVED EAM DEPLOYED IN CISLUNAR SPACE BEFORE 2020. THIS SPACECRAFT WILL BE THE FIRST BUILDING BLOCK IN SUPPORTING BOTH COMMERCIAL MARKETS AND GOVERNMENT OBJECTIVES. THE PROPOSED EFFORT FOR THIS NEXTSTEP BAA PHASE I, INVOLVES DEFINING AN EAM ARCHITECTURE AND CONCEPT OF OPERATIONS (CONOPS) THAT ADDRESSES COMMERCIAL MARKETS AND NASA EXPLORATION OBJECTIVES, TECHNOLOGY MATURATION PLANNING AND INFRASTRUCTURE DEVELOPMENT, AND TO IDENTIFY TECHNOLOGIES THAT CAN BE IMPLEMENTED AND DEMONSTRATED IN THE ISSILEO ENVIRONMENT WITHIN THE NEXT THREE YEARS. TO MATURE HABITATION TECHNOLOGIES, THE CONTRACTOR WILL IDENTIFY STATE OF THE ART (SOA) TECHNOLOGIES ACROSS NASA TECHNOLOGY AREAS (TAS) DEFINED IN THE NASA TECHNOLOGY ROADMAP. FOCUS WILL BE ON MATURATION OF THE FOLLOWING TECHNOLOGIES ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEMS ENVIRONMENTAL MONITORING SAFETY AND EMERGENCY RESPONSE AND HABITATION THERMAL CONTROL SYSTEMS AUTONOMOUS HABITATION SYSTEMS NAVIGATION SYSTEMS MANAGEMENT DOCKING AND CAPTURE MECHANISMS AND DEPLOYABLE HABITATION ELEMENTS