HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL

WATER PRODUCTION SERVICES ON-BOARD THE INTERNATIONAL SPACE STATION (ISS)

IGF::OT::IGF THE CONTRACTOR SHALL PROVIDE AN IMPROVED UNIVERSAL WASTE MANAGEMENT SYSTEM (UWMS). UWMS SUPPORTS THE ADVANCED EXPLORATION SYSTEMS (AES) PROGRAM'S GOALS OF DEVELOPING AND TESTING NEW TECHNOLOGIES TO SUPPORT HUMAN LONG-TERM, DEEP SPACE EXPLORATION. THE UWMS IS MEANT TO PROVIDE A ROBUST, RELIABLE AND FLEXIBLE SOLUTION TO VARIED MISSION PROFILES. PROCUREMENT OF THE UWMS SUPPORTS THE ADVANCED EXPLORATION SYSTEMS (AES) PROGRAM'S GOALS OF DEVELOPING AND TESTING NEW TECHNOLOGIES TO SUPPORT HUMAN LONG-TERM, DEEP-SPACE EXPLORATION. THE UWMS IS MEANT TO PROVIDE A ROBUST, RELIABLE, AND FLEXIBLE SOLUTION TO VARIED MISSION PROFILES. DEMONSTRATING THE UWMS FIRST ON THE ISS REDUCES RISK FOR FOLLOW ON UNITS SUPPORTING HUMAN LONG-TERM, DEEP-SPACE EXPLORATION. NASA RESEARCH ANNOUNCEMENT (NRA) NNJ13ZBG001N WAS RELEASED ON NOVEMBER 14, 2012 SOLICITING PROPOSALS FOR EXPLORATION TECHNOLOGY DEMONSTRATIONS AND NATIONAL LAB UTILIZATION ENHANCEMENTS. ONE OF THE NRA AREAS OF INTEREST WAS HUMAN WASTE MANAGEMENT SYSTEMS WITH THE FOLLOWING CAPABILITIES: CAPABLE OF COLLECTING URINE, FECAL, MENSTRUAL, AND EMESIS WASTE IN A MICROGRAVITY ENVIRONMENT AND CONTROLLING ODOR. ALLOW COMMONALITY BETWEEN DIFFERENT VEHICLES WITH MINOR MAINTENANCE OR RECONFIGURATION. SUPPORT MISSIONS BETWEEN ONE WEEK AND INDEFINITE LENGTH WITH PERIODIC QUIESCENT PERIODS. ALLOW TRANSFER OF COLLECTED WASTE TO BOTH STORAGE AND DOWNSTREAM PROCESSING. SYSTEM SHALL HAVE VERY LOW AIR INCLUSION IN THE URINE BE A SIGNIFICANT IMPROVEMENT IN INSTALLED EQUIPMENT MASS

SUSTAINING ENGINEERING SERVICES TO SUPPORT THE SABATIER SYSTEMS ON-BOARD THE INTERNATIONAL SPACE STATION

PRELIMINARY DEFINITION OF THE ISS WATER PROCESSOR ASSEMBLY (WPA) AND OXYGEN GENERATOR ASSEMBLY

IGF::OT::IGF THE HSSSI BAA IDENTIFIED HABITATION SYSTEMS AS A KEY LONG TERM CAPABILITY AREA THAT COULD POTENTIALLY SIGNIFICANTLY BENEFIT FUTURE HUMAN SPACE EXPLORATION. THE BAA SEEKS CONCEPTS AND TECHNOLOGY INVESTIGATION FOR AN INITIAL HABITATION CAPABILITY IN CISLUNAR SPACE WITH EXTENSIBILITY FOR IN-SPACE TRANSIT HABITATION SUCH AS THOSE BEING CONSIDERED BY NASA UNDER ITS EXPLORATION AUGMENTATION MODULE(S) (EAM) OR THE CAPABILITIES THAT ENABLE A POTENTIAL USE OF COMMERCIAL LOW EARTH ORBIT (LEO) HABITATION CAPABILITIES COUPLED WITH GOVERNMENT-PROVIDED EXPLORATION IN-SPACE HABITATION CAPABILITIES IN CISLUNAR SPACE. ONE AREA OF HABITATION PROPOSALS COULD INCLUDE CONCEPT STUDIES OR ENHANCEMENTS AND TESTING OF EXPLORATION ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEMS (ECLSS), SUCH AS ATMOSPHERE REVITALIZATION AND MONITORING, WATER PROCESSING, LIGHTING, AND FIRE DETECTION. THIS PROPOSAL IS FOR A PHASE 1 EFFORT EXECUTED WITH A FIXED PRICE CONTRACT BASED ON MILESTONE ACHIEVEMENTS DURING A ONE YEAR BASE EFFORT WITH POTENTIAL FOLLOW ON PHASES.

THERMAL AMINE SYSTEM DESIGN, DELIVERY, AND SUSTAINING

MECHANICAL REFRIGERATION SYSTEM TESTING AND EVALUATION

VENTILATION LOOP FANS FOR THE EXPLORATION PORTABLE LIFE SUPPORT SYSTEM

CYLINDRICAL RAPID CYCLE AMINE SERVICES

IGF::OT::IGF GFPHASE CHANGE MATERIAL HEAT SINK

HYDROPHILIC COATING REFORMULATION STUDY (UTAS)

IGF::OT::IGF FIRM FIXED PRICE CONTRACT FOR THE DEVELOPMENT AND DELIVERY OF AN AMBIENT CATALYSTIC REACTOR CATALYST

4506798919!SEPARATOR

ON-SITE TECHNICAL SUPPORT

AFCC MEMORY LOADER/VERIFIER AND LAPTOP

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

IGF::OT::IGF SABATIER SE CALL ORDER 1

4507272857!METER,FLO

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

IGF::OT::IGF THERMAL AMINE REMOVAL SYSTEM FEASIBILITY STUDY

IGF::OT::IGF PROVIDE THE NASA LYNDON B. JOHNSON SPACE CENTER (JSC) WITH CONTINUED SUSTAINING ENGINEERING AND ANOMALY RESOLUTION SERVICES USING AN EXISTING SABATIER-REACTION BASED SYSTEM FOR THE INTERNATIONAL SPACE STATION.

IGF::OT::IGF THE NASA AUTHORIZATION ACT OF 2010 (P.L. 111-267) AUTHORIZES THE NASA OFFICE OF THE CHIEF TECHNOLOGIST (OCT) TO DEVELOP TECHNOLOGIES IN SUPPORT OF SPACE EXPLORATION. TO THIS END, OCT HAS CREATED THE GAME CHANGING DEVELOPMENT (GCD) PROGRAM WITHIN THE SPACE TECHNOLOGY PROGRAM (STP). THE GCD PROGRAM PRIMARILY FOCUSES ON MATURATION OF KEY TECHNOLOGIES ACROSS THE MID-TECHNOLOGY READINESS LEVELS (TRL), NAMELY TRL 3-5. FUTURE NASA MISSIONS REQUIRE THE DEVELOPMENT OF ADVANCED THERMAL CONTROL TECHNOLOGIES. MORE SPECIFICALLY, NASA IS INTERESTED IN THE DEVELOPMENT OF VARIABLE HEAT REJECTION (VHR) TECHNOLOGIES APPLICABLE TO THESE EXPLORATION MISSIONS. THE NASA HUMAN SPACEFLIGHT STUDIES HAVE IDENTIFIED VHR THERMAL CONTROL SYSTEMS AS A KEY CAPABILITY REQUIRED FOR EXTENDING HUMAN PRESENCE THROUGHOUT THE SOLAR SYSTEM. IN ADDITION, THE NEED FOR THESE TECHNOLOGIES WAS CAPTURED WITHIN THE RELEVANT NASA SPACE TECHNOLOGY ROADMAP (TA-14, THERMAL MANAGEMENT SYSTEMS) AND INNOVATIVE COMPONENTS AND LOOP ARCHITECTURES WERE IDENTIFIED AS THE SECOND MOST IMPORTANT TECHNICAL CHALLENGE WITHIN THAT ROADMAP. FINALLY, THE VHR INITIATIVE RESPONDS TO THE TECHNOLOGIES IN THE NATIONAL RESEARCH COUNCIL'S RECOMMENDATIONS TO THE NASA TECHNOLOGY ROADMAPS. THE SUBJECT PURCHASE ORDER IS THE RESULT OF TWO PROPOSALS SUBMITTED BY HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC. THAT WERE SELECTED FOR AWARD UNDER THE NASA RESEARCH ANNOUNCEMENT (NRA) NNL12A3001N ENTITLED "GAME CHANGING OPPORTUNITIES IN TECHNOLOGY DEVELOPMENT (GCOTD) - 2012" APPENDIX C, TECHNOLOGY DEVELOPMENT FOR VARIABLE HEAT REJECTION (VHR). THE NRA SOLICITATION SOUGHT PROPOSALS FOR THE STUDY OF ADVANCED VARIABLE HEAT REJECTION TECHNOLOGIES TO ADDRESS A DIFFICULT DESIGN CHALLENGE FACING FUTURE NASA EXPLORATION MISSIONS. THE VHR DEVELOPMENT EFFORT IS ANTICIPATED TO OCCUR IN FOUR PHASES. DURING EACH PHASE, THE TECHNOLOGY READINESS LEVEL (TRL) OF THE SELECTED TECHNOLOGIES WILL BE ADVANCED AND THE CULMINATION OF PHASE IV WILL RESULT IN TRL 5/6 HARDWARE. PHASE I, IS THE FORMULATION PHASE, AND WILL INCLUDE AN ANALYTICAL STUDY TO DEMONSTRATE THE FEASIBILITY AND VIABILITY OF THE PROPOSED TECHNOLOGY. ONLY PHASE I IS PRESENTLY APPROVED BY THE GCD PROGRAM MANAGEMENT AND WAS SOLICITED UNDER APPENDIX C. AT THE END OF THE FORMULATION PHASE, THE STUDY RESULTS WILL BE REVIEWED ALONG WITH PROGRAMMATIC CONSIDERATIONS TO DETERMINE WHETHER THE PROJECT WILL ENTER IMPLEMENTATION, PHASES II THROUGH IV.

IGF::OT::IGF SABATIER SUSTAINING SERVICES FOR MAY 2015.

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES FOR JULY 2015.

NASA PRESENTLY PROVIDES THE HIGH PURITY, HIGH PRESSURE OXYGEN USED BY THE EVA MOBILITY UNIT (EMU, OR SPACESUIT) WITH SHUTTLE DERIVED OXYGEN. THE OXYGEN IS LAUNCHED ON THE SHUTTLE AS A CRYOGENIC FLUID, TRANSFERRED TO THE INTERNATIONAL SPACE STATION (ISS) AS A MODERATE PRESSURE GAS USING A TRANSFER HOSE, FURTHER COMPRESSED USING AN ONBOARD COMPRESSOR, AND STORED IN LARGE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. AFTER THE SHUTTLE RETIRES, ISS WILL CONTINUE TO CONDUCT EVAS AND NEED A NEW SUPPLY OF HIGH PRESSURE HIGH PURITY OXYGEN. THE ISS USES WATER ELECTROLYSIS TO PROVIDE LOW PRESSURE OXYGEN FOR METABOLIC CONSUMPTION. NASA IS DEVELOPING A SYSTEM TO FILTER CABIN AIR, CONCENTRATE A STREAM OF LOW PRESSURE HIGH PURITY OXYGEN, COMPRESS THE OXYGEN WITH AN ON BOARD COMPRESSOR, AND STORE THE OXYGEN IN THE EXTERNAL HIGH PRESSURE OXYGEN STORAGE TANKS. THE OXYGEN PURITY REQUIREMENT FOR USE IN THE EMU IS GREATER THAN 99.5% PURITY. THE DELIVERY RATE TARGET IS 5 LBS O2 PER DAY. THE SEPARATION SYSTEM NEEDS TO OPERATE IN THE ISS ENVIRONMENT. ONE OF THE APPROACHES FOR OXYGEN CONCENTRATION USES A TWO BED, SINGLE STAGE, VACUUM PRESSURE SWING ADSORPTION (VPSA) SYSTEM. NASA HAS COLLECTED PERFORMANCE DATA FROM TWO DIFFERENT VPSA DEVICES. THE FIRST DEVICE IS A SUB SCALE PROTOTYPE UNIT, THAT MEETS O2 PURITY REQUIREMENTS, BUT PRODUCES LESS THAN 5 LBS PER DAY. THE SUBSCALE DEVICE USES A SORBENT DESCRIBED IN US PATENT 6,432,170. THE PATENT HOLDERS DO NOT HAVE ADDITIONAL SORBENT MATERIAL AVAILABLE FOR USE BY NASA. BECAUSE NASA NEEDS A RELATIVELY SMALL AMOUNT OF SORBENT (NOMINALLY 250 LBS FOR THE ENTIRE SYSTEM, INCLUDING RESERVE MATERIAL), THE PATENT HOLDERS CANNOT PRODUCE A COMMERCIALLY VIABLE BATCH OF SORBENT SPECIFICALLY FOR NASA. NASA S SECOND PROTOTYPE SYSTEM IS A FULL SCALE, TWO BED, SINGLE STAGE, VPSA SYSTEM CAPABLE OF PRODUCING MORE THAN 5 LBS OF OXYGEN PER DAY. BECAUSE OF SORBENT LIMITATIONS, THIS SYSTEM IS NOT CAPABLE OF MEETING THE 99.5% O2 PURITY REQUIREMENT. NASA SEEKS TO TEST THE PERFORMANCE OF CANDIDATE SORBENTS IN THE 5 LB PER DAY PROTOTYPE UNIT. ADDITIONALLY, NASA SEEKS TO ASSESS KEY SORBENT PERFORMANCE CHARACTERISTICS. NASA IS WILLING TO CONSIDER ANY SORBENTS THAT ARE CAPABLE OF PRODUCING AN OXYGEN STREAM WITH GREATER THAN 99.5% PURITY WHEN CONCENTRATING STANDARD AIR. ONE APPROACH WOULD BE TO USE THE MATERIAL SPECIFIED IN US PATENT 6,432,170, ASSIGNED TO AIR PRODUCTS AND CHEMICALS, INC. (CONTACT JEFF KNOPF @ KNOPFJA@APCI.COM). NASA IS ALSO INTERESTED IN OTHER SORBENTS CAPABLE OF SEPARATING HIGH PURITY OXYGEN FROM AIR. IF TEST RESULTS ARE FAVORABLE, NASA MAY PURCHASE SORBENT FOR OXYGEN SEPARATION SYSTEMS. THE NOMINAL BATCH SIZE OF THIS ORDER IS 250 LBS (MAYBE MORE, MAYBE LESS, DEPENDING ON THE COST OF THE MATERIAL). NASA INTENDS TO AWARD (UP TO THREE) PURCHASE ORDER CONTRACTS. NASA WILL OBTAIN A RESEARCH REPORT AS A PRODUCT. THE TECHNICAL ACTIVITIES WILL REQUIRE THE CONTRACTOR TO DEVELOP AND CHARACTERIZE SORBENTS CAPABLE OF PRODUCING HIGH PURITY OXYGEN FROM AIR.

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

REPAIR OF AIRCRAFT PARTS - SERVICE CONTRACT ACT N/A.

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES FOR SEPTEMBER 2015.

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES FOR OCTOBER 2015.

IGF::OT::IGF SUSTAINING ENGINEERING SERVICES FOR AUGUST 2015.

IGF::OT::IGF SUSTAINING ENGINEERING SUPPORT SERVICES

NP2000 SE SPARES KIT

IGF::OT::IGF SUSTAINING ENGINEERING SERVICES FOR NOVEMBER 2015.

4507432996!VALVE ASS

NEXTSTEP APPENDIX D (IN-SITU RESOURCE UTILIZATION) CONTRACT FOR UNITED TECHNOLOGIES CORPORATION AEROSPACE SYSTEMS (UTAS)

GSE

NAVY AVIATION

FMS NIS RQMT

PURCHASE ONE (1) THERMAL CATALYST

REPAIR OF AIRCRAFT PARTS - SERVICE CONTRACT ACT N/A.

4508081620!CIRCUIT C

4508068584!SWITCH,PR

REPLACE THE ASU TANK LEVEL D/P TRANSDUCE

IGF::OT::IGF REPAIR OF AIRCRAFT PARTS - SERVICE CONTRACT ACT N/A.

CASE ASSY

QTY 16 SYLINDER ASSEMBLIES

NEXTSTEP APPENDIX D (IN-SITU RESOURCE UTILIZATION) CONTRACT FOR UNITED TECHNOLOGIES CORPORATION AEROSPACE SYSTEMS (UTAS)