HONEYWELL INTERNATIONAL, INC.

SPARROW RFROG

WFIRST PROJECT LAUNCH LOCK AND VIBRATION ISOLATION SYSTEM (LLVIS)

IGF::OT::IGF - SPARROW ACCELEROMETER

HP/30 CARBON DIOXIDE REMOVAL BY IONIC LIQUID SORBENT

BAA CALL 0012 - MINIATURE P-N-P CONTROL SYSTEM

WFIRST REACTION WHEEL ASSEMBLY

SEE SECTION J - ATTACHMENTS FOR THE COMPLETE STATEMENT OF WORK.

RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)

IGF::OT::IGF OTHER FUNCTIONS DISTURBANCE MONITORING PACKAGE

EIGHT (8) PANEL MOUNTED BREATHER REGULATORS (VALVE, OXYGEN MASK, AIRCRAFT), PART NUMBER SPC-77301418-0001, DRAFT 2A

KEDALION AVIONICS SUPPORT

THE GOVERNMENT IS SEEKING TECHNOLOGICAL APPROACHES FOR IMPROVING FAR TARGET LOCATION (FTL) FOR FUTURE TARGETING SYSTEMS. FTL IS A KEY ELEMENT OF THE US ARMY S FORCE OPERATING CAPABILITIES (FOC) DOCTRINE TO SEE, UNDERSTAND, AND ACT FIRST AND FOREMOST ON THE BATTLEFIELD. PRECISE FTL DATA PROVIDES TODAY S SOLDIER WITH ESSENTIAL INFORMATION PERTAINING TO DIRECT AND INDIRECT FIRE, SURVEILLANCE, AND MANEUVER MISSIONS, WHERE RELIABLE AND ACCURATE SITUATIONAL AWARENESS (SA) IS VITALLY IMPORTANT FOR DISMOUNTED MILITARY OPERATIONS.

200602!000439!1700!N00014!OFFICE OF NAVAL RESEARCH !N0001406C0001 !A!N! !N! ! !20051212!20080930!148371875!148371875!139691877!N!HONEYWELL INTERNATIONAL INC !19019 N 59TH AVE !GLENDALE !AZ!85308!27820!013!04!GLENDALE !MARICOPA !ARIZONA !+000000100000!N!N!000000000000!AD93!RDTE/OTHER DEFENSE-ADV TECH DEV !S1 !SERVICES !000 !* !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!N!U!2!999!E! !Z!Y!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!C!N! ! ! ! !1714!N00014!0001! !

THE CONTRACTOR SHALL PERFORM SPACE INTEGRATED GPS/INS (SIGI) WORK.

KEDALION AVIONICS SUPPORT

KEDALION AVIONICS SUPPORT

ISS GPS EXPLORATION TEST SUPPORT

THE CONTRACTOR SHALL PERFORM ISS GN&C ANALYSIS WORK.

ISS GPS EXPLORATION TEST SUPPORT

KEDALION AVIONICS SUPPORT

KEDALION LAB SUPPORT

CARBON DIOXIDE REMOVAL BY IONIC LIQUID SORBENT FOR MOBILITY (CDRILS-M)

HONEYWELL AVIONICS SUPPORT

IGF::OT::IGF THE PURPOSE OF THIS MODIFICATION IS TO ADD TASK ORDER 6 TO THE CONTRACT. PERIOD OF PERFORMANCE: 01/02/2017-7/03/2017

DISPLAY PROTOTYPE TO PRODUCTION PATHFINDER

CONTRACTOR SHALL PROVIDE TECHNICAL AND VENDOR COORDINARION OF THE HONEYWELL AVIONICS DEVELOPMENT PRODUCTS NASA KEDALION USE.

EXPLORATION SYSTEMS MISSION DIRECTORATE LUNAR SURFACE SYSTEMS CONCEPTS STUDY THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA) IS CURRENTLY STUDYING LUNAR OUTPOST ARCHITECTURE CONCEPTS, INCLUDING HABITATION, MOBILITY AND COMMUNICATION SYSTEMS, TO SUPPORT U.S. LUNAR EXPLORATION AND SCIENCE OBJECTIVES. NASA IS IN THE PROCESS OF DEFINING FUNCTIONAL CAPABILITIES AND CONCEPTS FOR ARCHITECTURAL ELEMENTS TO PROVIDE CORE CAPABILITIES. DESCRIPTION OF STUDY AREAS ALTERNATIVE PACKAGING OPTIONS OBJECTIVE THE PRIMARY OBJECTIVE OF THIS STUDY IS TO PRODUCE ALTERNATIVE PACKING OPTIONS THAT ELIMINATE OR MINIMIZE WASTE GENERATION FROM PACKING MATERIALS AND ALLOW OPTIMAL UTILIZATION OF AVAILABLE STOWAGE VOLUME. POTENTIAL ALTERNATIVES CAN INCLUDE CONCEPTS THAT DO NOT REQUIRE PACKING MATERIAL AT ALL OR THAT EMPLOY PACKING MATERIALS THAT HAVE SECONDARY USES. A THIRD, BUT LESS DESIRABLE, APPROACH WOULD BE PACKING MATERIALS WHOSE VOLUME IS REDUCED FOLLOWING USE BUT WHICH STILL BECOME WASTE. ALL OPTIONS MUST SATISFY APPLICABLE REQUIREMENTS FOR INITIAL PACKING FUNCTION, MUST STRIVE TO MINIMIZE THE MASS OF THE PACKING MATERIALS, AND MUST COMPLY WITH OTHER SPACEFLIGHT REQUIREMENTS SUCH AS FLAMMABILITY AND OFFGASSING. AN ADDITIONAL GOAL IS THAT THE MASS OF PACKING MATERIAL NOT EXCEED THE MASS OF THE ITEM, OR ITEMS, BEING PACKED. BACKGROUND HISTORICALLY, PACKING MATERIALS HAVE BEEN EMPLOYED TO PROTECT STOWABLE HARDWARE ITEMS DURING ASCENT FROM THE AMBIENT VIBROACOUSTIC ENVIRONMENT. EXAMPLES OF ITEMS THAT ARE PACKED IN THIS WAY INCLUDE SPARE SPACECRAFT HARDWARE COMPONENTS, TOOLS, SCIENTIFIC INSTRUMENTS, FOOD AND PHOTOGRAPHIC EQUIPMENT. THESE PACKING MATERIALS OCCUPY A SIGNIFICANT FRACTION OF THE AVAILABLE STOWAGE VOLUME. ADDITIONALLY, THESE PACKING MATERIALS ACCOUNT FOR A VERY SUBSTANTIAL PROPORTION OF THE WASTE STREAM THAT EVOLVES DURING A MISSION AS THE STOWED ITEMS ARE UTILIZED AND THE PACKING MATERIAL NO LONGER SERVES A PURPOSE. THE END RESULT IS CONSUMPTION OF STOWAGE VOLUME BY MATERIAL THAT ENDS UP AS WASTE. TECHNICAL REQUIREMENTS TOPIC-SPECIFIC REQUIREMENTS TO BE ADDRESSED IN THE ORAL AND WRITTEN CONTRACT DELIVERABLES, SPECIFIED IN PARAGRAPH 8 OF SECTION IX, INCLUDE: 1. DEFINING THE PROPOSED ALTERNATIVE OPTIONS 2. ADDRESSING COMPLIANCE WITH FUNCTIONAL AND COMPATIBILITY REQUIREMENTS 3. DEFINING THE UNIT MASS OF PROPOSED MATERIALS, AND 4. DEFINING SECONDARY USES OF MATERIALS, AS APPLICABLE. MINIMUM FUNCTIONALITY HABITATION ELEMENT OBJECTIVE THE PRIMARY OBJECTIVE OF THIS STUDY IS TO PRODUCE A CONCEPTUAL DESIGN FOR A MINIMUM FUNCTIONALITY HABITATION ELEMENT BASED ON A MINIMUM SET OF FUNCTIONS THAT ARE REQUIRED TO PERFORM THE REFERENCE MISSION. THE MINIMUM FUNCTIONALITY HABITATION ELEMENT INCLUDES BASIC REQUIRED SAFETY FEATURES BUT DOES NOT PROTECT FOR CONTINGENCY SITUATIONS.

INTEGRATED POWER AVIONICS AND SOFTWARE WAYPOINT DEMONSTRATION

PURCHASE MATERIALS REQUIRED TO CONVERT 3 CRV SIGI UNITS TO ISS FLIGHT UNITS

KEDALION LAB SUPPORT

IGF::OT::IGF CRV SIGI RECONFIGURATION TO ISS SIGI FLIGHT UNITS

PURPOSE- THIS STATEMENT OF WORK (SOW) DEFINES THE TASKS REQUIRED TO SUPPORT THE DESIGN OF A RUGGEDIZED FIBER OPTIC SENSOR SYSTEM FOCUSING ON UTILIZING HARDWARE FROM THE CURRENT DESIGN. THE STUDY WILL FOCUS ONLY ON MODIFICATIONS NECESSARY FOR THE SYSTEM TO SURVIVE MINOTAUR LAUNCH ENVIRONMENTS. THIS STUDY WILL ALSO DETERMINE THE DESIGN MODIFICATIONS NECESSARY FOR THE CURRENT HARDWARE TO SURVIVE A FLIGHT EXPERIMENT MISSION IN LEO ORBIT LASTING LESS THAN 12 MONTHS. A SYSTEMS APPROACH WILL BE APPLIED TO THE FIBER OPTIC SENSOR SYSTEM IN ORDER TO DETERMINE THE REQUIRED CHANGES NECESSARY FOR THE SYSTEM TO OPERATE IN SPACE. THE CONTRACTOR SHALL PROVIDE LABOR AND MANAGEMENT NECESSARY TO ADEQUATELY PERFORM THE SPECIFIC TASKS BELOW. SCOPE OF WORK- COMPLIANCE WITH THE REQUIREMENTS STATED HEREIN, SHALL BE THE RESPONSIBILITY OF THE CONTRACTOR. THE CONTRACTOR SHALL FURNISH, UNLESS OTHERWISE SPECIFIED, ALL NECESSARY PERSONNEL, FACILITIES, AND EQUIPMENT TO CONDUCT THE STUDY TASKS SPECIFIED HEREIN, IN ACCORDANCE WITH THIS SOW AND THE SPECIFICATIONS, DOCUMENTS, AND SCHEDULES STATED AND/OR REFERENCED HEREIN. TECHNICAL GUIDANCE - TECHNICAL GUIDANCE TO BE PROVIDED TO THE CONTRACTOR BY THE NASA DRYDEN FLIGHT RESEARCH CENTER WILL CONSIST OF PROVIDING THE CONTRACTOR THE FIBER SENSOR SYSTEM HARDWARE ALONG WITH SPECIFICATIONS AND OPERATING INSTRUCTIONS. TASK DESCRIPTIONS - PROGRAM MANAGEMENT - THE CONTRACTOR SHALL PROVIDE CENTRALIZED PROJECT MANAGEMENT TO EXECUTE THE TASKS DESCRIBED IN THIS SOW. A PROJECT MANAGER SHALL BE APPOINTED WHO SHALL POSSESS SINGULAR AUTHORITY TO PLAN AND DIRECT THE REQUIRED EFFORT. SYSTEM REQUIREMENTS FOR LAUNCH SURVIVAL - THE CONTRACTOR SHALL GENERATE AND SUBMIT REQUIREMENTS NECESSARY FOR THE FIBER OPTIC SENSOR SYSTEM SUPPLIED BY NASA DRYDEN FLIGHT RESEARCH CENTER TO SURVIVE A LAUNCH ENVIRONMENT. THE CONTRACTOR SHALL USE MINOTAUR LAUNCH ENVIRONMENT TO DEVELOPMENT BASELINE REQUIREMENTS. CONCEPT DESIGN FOR LAUNCH SURVIVAL - THE CONTRACTOR SHALL IDENTIFY EXPECTED PACKAGING AND SYSTEM MODIFICATIONS NECESSARY FOR THE EXISTING FIBER OPTIC SENSOR SYSTEM TO MEET THE LAUNCH REQUIREMENTS DEVELOPED IN 9.2. THE CONCEPT DESIGN WILL ONLY CONSIDER MODIFICATIONS TO THE EXISTING HARDWARE NECESSARY FOR ITS SURVIVAL DURING LAUNCH. A CONCEPT DESIGN SHALL INCLUDE TRADE STUDIES PERFORMED TO ARRIVE AT THE SELECTED DESIGN. A REVIEW OF SYSTEM REQUIREMENTS SHALL BE AN INTEGRAL COMPONENT OF THE CONCEPT DESIGN. SYSTEM ARCHITECTURE FOR SHORT LEO MISSION - THE CONTRACTOR SHALL DEVELOP PRELIMINARY SPECIFICATIONS FOR A FIBER OPTIC SENSOR SYSTEM TO SURVIVE A LEO MISSION LASTING LESS THAN 12 MONTHS. THE CONTRACTOR SHOULD SUGGEST LOW COST MODIFICATIONS NECESSARY FOR THE EXISTING FIBER OPTIC SENSING SYSTEM TO MEET THESE PRELIMINARY REQUIREMENTS. THE SUGGESTED MODIFICATIONS SHOULD BE IN LINE WITH A FLIGHT EXPERIMENT MISSION. SYSTEM ARCHITECTURE FOR OPERATIONAL LEO MISSION - THE CONTRACTOR SHALL DEVELOP AN ESTIMATE OF ADDITIONAL FUNDING NEEDED FOR A SUBSEQUENT PHASE FOCUSING ON DEVELOPING SPECIFICATIONS AND DESIGN MODIFICATIONS NECESSARY FOR A FIBER OPTIC SENSOR SYSTEM TO SURVIVE AN OPERATIONAL LEO MISSION WITH A MAXIMUM LIFE OF 8 YEARS. THE CONTRACTOR SUGGESTS MODIFICATIONS NECESSARY FOR THE EXISTING FIBER OPTIC SENSING SYSTEM TO MEET THESE REQUIREMENTS. MODIFICATIONS MAY REQUIRE SIGNIFICANT ARCHITECTURAL CHANGES TO THE CURRENT FIBER OPTIC SENSING SYSTEM.

IMA TRAINING MATERIALS AND COURSE FOR IPAS PROJECT SPT

SUPPORT OF FAILURE ANALYSIS OF ISS SIGI S/N 14 ON ISS AND THE ASSOCIATED RECOVERY PLAN.

IGF::OT::IGF CRV SIGI RECONFIGURATION TO ISS SIGI FLIGHT UNITS

IGF::OT::IGF INTERNATIONAL SPACE STATION (ISS) GPS SPECIALIZED EXPLORATION TEST SUPPORT

IGF::OT::IGF HONEYWELL DO #4 ISS SIGI S/N 0013 REPAIR

2011 EVA DRATS TESTING PROGRAM

ISS GPS EXPLORATION TEST SUPPORT

PLUG-AND-PLAY SOFTWARE FOR ATTITUDE CONTROL SYSTEMS

IGF::OT::IGF ISS GPS

ENGINEERING SERVICES

RING LASER GYRO

SPECIAL STUDIES/ANALYSIS- AERONAUTICAL/SPACE

GENERAL ENGINEERING SUPPORT TO THE INTERNATIONAL SPACE STATION (ISS) SPACE INTEGRATED GLOBAL POSITIONING SYSTEM/ INERTIAL NAVIGATION SYSTEM(SIGI)

HONEYWELL UPDATE A NRC CARD, PROVIDED UNDER THE KEDALION PROGRAM, TO THE CURRENT CONFIGURATION

SCALABLE HOMELAND INNOVATIVE ENTERPRISE LAYERED DEFENSE (SHIELD) INITIAL ORDER.

THE CONTRACTOR SHALL PROVIDE ALL NECESSARY MATERIALS, LABOR, EQUIPMENT AND FACILITIES INCIDENTAL TO THE PERFORMANCE OF THIS REQUIREMENT IN ACCORDANCE WITH THE TERMS OF THE ORDER.

ISS GPS EXPLORATION TEST SUPPORT

DESIGN OF A BREATHING OXYGEN REGULATOR SYSTEMS FOR THE LOW BOOM FLIGHT DEMONSTRATOR