SPACE VEHICLE COMPONENTS

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.

DESCOPE OF THE WOMA REQUIREMENT WAS ISSUED AS A FULL AND OPEN COMPETITIVE PROCUREMENT TO DESIGN, ANALYZE, DEVELOP, FABRICATE, INTEGRATE, TEST, AND EVALUATE THE WIDE FIELD INSTRUMENT (WFI) OPTO-MECHANICAL ASSEMBLY (WOMA) FOR THE WIDE FIELD INFRARED SURVEY TELESCOPE (WFIRST) MISSION. IN ADDITION, IT DEFINES THE TASKS NECESSARY TO SUPPORT THE SUBSEQUENT INTEGRATION, TEST, EVALUATION, AND VALIDATION OF THE WFI. IT DEFINES THE POST-DELIVERY SUPPORT TO PAYLOAD AND OBSERVATORY INTEGRATION AND TEST, AND TO PRE-LAUNCH, LAUNCH AND COMMISSIONING ACTIVITIES AT THE MISSION OPERATIONS CENTER (MOC) AND TO SUPPLY AND MAINTAIN THE INSTRUMENT GROUND SUPPORT EQUIPMENT (GSE).

THE CONTRACTOR FURNISHES ALL THE NECESSARY PERSONNEL, FACILITIES, SERVICES, EQUIPMENT, AND MATERIALS TO DESIGN, FABRICATE, INTEGRATE, TEST, AND DELIVER THE SPACECRAFT BUS, AND PROVIDE SERVICES SUCH AS INTEGRATION AND TEST OF THE RSV AT GSFC AND PERFORMANCE OF ON-ORBIT ACTIVITIES FOR THE INITIAL RESTORE-L REFUELING CAMPAIGN IN MID-2020. SINCE THE CONTRACTOR IS PROVIDING THE SPACECRAFT BUS, NASA INVOLVEMENT WILL BE TAILORED TO BALANCE THE LEVELS OF OVERSIGHT VS. INSIGHT NEEDED TO ASCERTAIN THE APPROPRIATE LEVEL OF RISK TO THE OVERALL MISSION.

MARS ASCENT PROPULSION SYSTEM (MAPS)

THE PURPOSE OF THIS MODIFICATION IS TO ADD INCREMENTAL FUNDING TO CLIN 3301 OF THE TASK ORDER. ALL OTHER TERMS AND CONDITIONS REMAIN UNCHANGED.

UPDATE STATEMENT OF WORK (SOW) SOLAR-SWIPS-SOW-0003, REVISION B REQUIREMENTS SPECIFICATION (SPEC)SOLAR-SWIPS-REQ-0010, REVISION A CONTRACT DELIVERABLE REQUIREMENTS LIST (CDRL) SOLAR-SWIPS-REQ-0010, REVISION A

THE PRINCIPAL PURPOSE OF THIS REQUIREMENT WITHIN THE SWFO PROJECT IS TO DESIGN, ANALYZE, DEVELOP, FABRICATE, INTEGRATE, TEST, CALIBRATE, EVALUATE AND SUPPORT LAUNCH AND ON-ORBIT CHECK-OUT OF THE SWIPS INSTRUMENT AS PART OF THE SWFO-L1 OBSERVATORY.

FUNDING ONLY ACTION FOR THE DESIGN, ANALYZE, DEVELOP, FABRICATE, INTEGRATE, TEST, VERIFY, EVALUATE, SUPPORT LAUNCH, SUPPLY AND MAINTAIN THE L1 SERIES SUPRATHERMAL ION SENSOR.

ROMAN SPACE TELESCOPE INSTRUMENT CARRIER (IC) LAUNCH LOCK AND VIBRATION ISOLATION SYSTEM (LLVIS)

ENHANCED POLAR SYSTEM RECAPITALIZATION - TWO PAYLOADS (P6&P7)

POLSIR SPACECRAFT

COMMERCIAL LIGHT DETECTION AND RANGING (LIDAR) SENSOR FOR THE ON-ORBIT SERVICING, ASSEMBLY, AND MANUFACTURING (OSAM-1) MISSION.

DESIGN, DEVELOPMENT, FABRICATION, ALIGNMENT, TESTING, VERIFICATION, DELIVERY, AND ASSOCIATED POST-DELIVERY SUPPORT SERVICES FOR THE LASER INTERFEROMETER SPACE ANTENNA (LISA) ENGINEERING TEST UNIT (ETU) TELESCOPE.

UCB SHALL BE DIRECTLY RESPONSIBLE FOR THE CONDUCT OF ALL PHASES AND ASPECTS OF THE SPAN-AI INSTRUMENT.

UNIVERSITY OF MICHIGAN SHALL BE DIRECTLY RESPONSIBLE FOR THE CONDUCT OF ALL PHASES AND ASPECTS OF THE MAGNETO-INDUCTIVE MAGNETOMETERS.

TASK ORDER 18 UNDER CLIN 4 OF THE SLS-USA CONTRACT 80GRC017C0008

SB SET-ASIDE, 42 OFFERS.BPA VENDORS SHALL PROVIDE FABRICATION SERVICES AT VENDORS SITE & SUPPLIES TO GSFC IN THEIR RESPECTIVE AREAS OF EXPERTISE FOR THE DEVELOPMENT OF INSTRUMENTS SPACE FLIGHT & NON-SPACEFLIGHT HARDWARE INTERCHANGEABLE PIECE PARTS.

TASK ORDER 17 UNDER CLIN 4 OF THE SLS-USA CONTRACT 80GRC017C0008

SB SET-ASIDE, 42 OFFERS.BPA VENDORS SHALL PROVIDE FABRICATION SERVICES AT VENDORS SITE & SUPPLIES TO GSFC IN THEIR RESPECTIVE AREAS OF EXPERTISE FOR THE DEVELOPMENT OF INSTRUMENTS SPACE FLIGHT & NON-SPACEFLIGHT HARDWARE INTERCHANGEABLE PIECE PARTS.

THE PURPOSE OF THIS MODIFICATION IS TO REVISE A CONTRACT CLAUSE IN SECTION I OF THE CONTRACT IN RESPONSE TO RECENT EXECUTIVE ORDERS. THIS MODIFICATION INCORPORATES A REVISED SECTION I INTO THE CONTRACT. ALL OTHER TERMS AND CONDITIONS REMAIN UNCHANGED

THERMAL AMINE SYSTEM DESIGN, DELIVERY, AND SUSTAINING

EO14042 - NASA HAS A REQUIREMENT FOR THE SPACE LAUNCH SYSTEM UNIVERSAL STAGE ADAPTER THAT WILL STRUCTURALLY CONNECT THE EXPLORATION UPPER STAGE TO THE ORION SPACECRAFT.