FedTALLY

Awards for “HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.

17 awards on this page · sorted by amount · page 3

Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
80JSC022F0136HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$58.89K
2022-05-232024-09-30541330UNIVERSAL WASTE MANAGEMENT SYSTEM (UWMS) URINE HOSE ASSEMBLY
NNH17CA07DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$58.52K
2017-06-142017-10-15541330IGF::OT::IGF UNDER THIS CALL, THE CONTRACTOR SHALL PERFORM AN ASSESSMENT OF THE SPARE UWMS COMPONENTS THAT WILL BE REQUIRED TO FULLY SUSTAIN ALL OPERATIONS OF THE UWMS AND THE CONTRACTOR WILL ALSO PERFORM AN ASSESSMENT OF THE UWMS CONSUMABLES REQUIRED.
NNJ10HA63PHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$57.11K
2010-03-102010-06-04541330PHASE CHANGE MATERIAL STUDY
80NSSC18F0739HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$52.55K
2018-03-062018-03-06541330OT:: THIS IS A DELIVERY ORDER FOR FOUR BATCHES OF SABATIER CATALYST.
NNM12AA31DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$39.94K
2012-03-022013-02-06541330IGF::OT::IGF ASSEMBLE OGS FOR TESTING
80NSSC18F1038HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$39.41K
2018-04-262018-04-26541330OT - SABATIER CATALYST
80JSC022F0165HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$39.3K
2022-06-242022-09-30541330INTERFACE TEST OF THE NASA CONDUCTIVITY MONITOR WITH THE UWMS
80HQTR18F0268HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$35.37K
2018-07-252018-10-19541330UNIVERSAL WASTE MANAGEMENT SYSTEM (UWMS) MULTI-PURPOSE CREW VEHICLE (MPCV)
N6554014P5237HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.Department of Defense$26.69K
2014-06-242014-09-30541690IGF::CT::IGF, CAMS IIA TRAINING ON SITE
NNJ12HB76DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$22.27K
2012-02-242012-08-24541330THE CREW AND THERMAL SYSTEMS DIVISION AT JSC HAS DEVELOPED AN INTERNATIONAL SPACE STATION (ISS) UTILIZATION PAYLOAD FOR EVALUATING THE CARBON DIOXIDE (CO2) CONTROL CAPABILITY WHICH UTILIZES A HAMILTON SUNDSTRAND DEVELOPED CARBON DIOXIDE AND MOISTURE REMOVAL AMINE SWING-BED SYSTEM (CAMRAS) IN CONJUNCTION WITH WATER AND AIR SAFE FEATURES IN ORDER TO ASSESS THE CARBON DIOXIDE REMOVAL CAPABILITY IN A SPACEFLIGHT ENVIRONMENT. THIS HS TECHNOLOGY HAS BEEN BASE-LINED FOR SEVERAL FUTURE VEHICLES AND THIS UTILIZATION PAYLOAD PROVIDES RISK MITIGATION FOR THESE VEHICLES. HAMILTON SUNDSTRAND PROVIDED DESIGN AND DEVELOPMENT SUPPORT DURING THE DEVELOPMENT PHASE OF THIS PAYLOAD. THIS INCLUDED AN INITIAL FEASIBILITY ASSESSMENT, REQUIREMENTS DEFINITION FOR THE CONTROL AND MONITORING SYSTEMS FOR THE SWINGBED, AND INITIAL DESIGN OF CONTROL AND POWER HANDLING MODULES FOR THE PAYLOAD. THIS PAYLOAD IS PRESENTLY ON ORBIT AND DURING ASSEMBLY OPERATIONS EXPERIENCED AN ANOMALY WHICH REQUIRES THE UNIQUE KNOWLEDGE AND SKILLS OF THE HAMILTON SUNDSTRAND SWINGBED DESIGN TEAM. THIS EFFORT CONSISTS OF EVALUATING SWINGBED PAYLOAD FAULT TREE ANALYSES, IDENTIFYING AND VERIFYING POTENTIAL ROOT CAUSES. THE CONTRACTOR S SUPPORT WILL ALSO BE REQUIRED TO DEVELOP AND EVALUATE RECOVERY PLANS TO ENSURE THE PROPOSED COURSE OF ACTION MEETS THE INTENT SPECIFIED. HAMILTON SUNDSTRAND S PROPRIETARY OWNERSHIP OF CAMRAS AND CURRENT ROLE IN THE HARDWARE DEVELOPMENT MAKE THEM THE ONLY CANDIDATE FOR THE WORK REQUIRED. HAMILTON SUNDSTRAND HAS PROPRIETARY RIGHTS TO A TECHNOLOGY THAT IS THE BASELINE CO2 AND HUMIDITY REMOVAL TECHNOLOGY FOR SEVERAL FUTURE SPACE VEHICLES. CO2 AND HUMIDITY CONTROL TECHNOLOGY IS ESSENTIAL TO THE SAFE OPERATION OF A SPACE CRAFT. THE CURRENT STATE OF THE ART (SOTA) IN CO2 REMOVAL FOR THE ISS IS A REGENERABLE SILVER OXIDE-BASED SORBENT THAT IS OF LIMITED DURATION AND IS NOT SUITABLE FOR ADVANCED PROGRAMS BECAUSE IT IS PROHIBITIVELY HEAVY (32 LB). THE CURRENT CANISTER AND VALVE CONFIGURATIONS WERE DEVELOPED SOLELY BY HAMILTON SUNDSTRAND UNDER INTERNAL R&D (IR&D) SINCE THE EARLY 2000S. THE CAMRAS WAS DEVELOPED BY HAMILTON SUNDSTRAND AND HAS BEEN UNDER TEST IN VARIOUS CONFIGURATIONS AT NASA S JOHNSON SPACE FLIGHT CENTER SINCE 2006.
NNJ12HE60DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$20.71K
2012-08-232013-03-29541330IGF::OT::IGF THE CREW AND THERMAL SYSTEMS DIVISION AT JSC HAS DEVELOPED AN INTERNATIONAL SPACE STATION (ISS) UTILIZATION PAYLOAD FOR EVALUATING THE CARBON DIOXIDE (CO2) CONTROL CAPABILITY WHICH UTILIZES A HAMILTON SUNDSTRAND DEVELOPED CARBON DIOXIDE AND MOISTURE REMOVAL AMINE SWING-BED (CAMRAS) IN CONJUNCTION WITH WATER AND AIR SAFE FEATURES IN ORDER TO ASSESS CO2 REMOVAL CAPABILITY IN A SPACEFLIGHT ENVIRONMENT. HAMILTON SUNDSTRAND PROVIDED DESIGN AND DEVELOPMENT SUPPORT DURING THE DEVELOPMENT PHASE OF THE PAYLOAD. THIS INCLUDED AN INITIAL FEASIBILITY ASSESSMENT, REQUIREMENTS DEFINITION FOR THE CONTROL AND MONITORING SYSTEMS FOR THE SWINGBED, AND INITIAL DESIGN OF CONTROL AND POWER HANDLING MODULES FOR THE PAYLOAD. THIS PAYLOAD IS PRESENTLY ON ORBIT AND, DURING INITIAL OPERATION, EXPERIENCED AN ANOMALY WHICH REQUIRES THE UNIQUE KNOWLEDGE AND SKILLS OF THE HAMILTON SUNDSTRAND CAMRAS DESIGN TEAM. THIS EFFORT CONSISTS OF EVALUATING SWINGBED PAYLOAD FAULT TREE ANALYSES, IDENTIFYING AND SUPPORTING VERIFICATION OF POTENTIAL ROOT CAUSES. THE CONTRACTOR S SUPPORT WILL ALSO BE REQUIRED TO DEVELOP AND EVALUATE RECOVERY PLANS TO ENSURE THE PROPOSED COURSES OF ACTION MEET THE INTENT SPECIFIED. TROUBLESHOOTING EFFORTS INCLUDE CONCENTRATING ON THE VALVE STEPPER MOTOR, INTERFACING ELECTRICAL HARNESSING AND MOTOR CONTROL DRIVE STAGE, HOWEVER ADDITIONAL ON-ORBIT TROUBLESHOOTING MAY BE NECESSARY TO YIELD FURTHER INFORMATION TO AID IN DIAGNOSIS AND REMEDIATION. HAMILTON SUNDSTRAND, AS THE ORIGINAL DEVELOPER OF THE AMINE SWINGBED, IS NECESSARY TO SUPPORT THE INVESTIGATION OF PAYLOAD FAILURES AS A PART OF A FAILURE ANALYSIS GROUP AS POTENTIAL CAUSES ARE RULED OUT. HAMILTON SUNDSTRAND HAS PROPRIETARY RIGHTS TO A TECHNOLOGY THAT IS THE BASELINE CO2 HUMIDITY REMOVAL TECHNOLOGY FOR SEVERAL FUTURE SPACE VEHICLES. CO2 AND HUMIDITY CONTROL TECHNOLOGY IS ESSENTIAL TO THE SAFE OPERATION OF A SPACE CRAFT. THE CAMRAS WAS DEVELOPED BY HAMILTON SUNDSTRAND AND HAS BEEN UNDER TEST IN VARIOUS CONFIGURATIONS AT NASA S JOHNSON SPACE CENTER SINCE 2006. THEIR HISTORICAL KNOWLEDGE OF DEVELOPING THIS TECHNOLOGY IS CRUCIAL TO THIS EFFORT.
NNM13AB40DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$19.98K
2013-01-012013-06-04541330IGF::CL::IGF ENGINEERING SUPPORT FOR THE OGA TESTBED RECOMBINER INVESTIGATION
NNJ12HB40DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$11.86K
2012-04-042013-04-08541330IGF::OT::IGF ENGINEERING SUPPORT FOR NASA PROOF OF CONCEPT TESTS AND DESIGN STUDY FOR SEARS(SPACESUIT EVAPORATOR ABSORBER RADIATOR) HEAT REJECTION CONCEPT
0006HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.Department of Defense$7.18K
2013-08-282013-09-24334516UNSCHEDULED MEETING TO BE HELD 24 SEPTEMBER 2013
NNJ12HA96DHAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration$02011-11-072012-11-10541330RAPID CYCLE AMINE
0001HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.Department of Defense$02017-11-172017-12-05541715START OF CONTRACT MEETING
NAS918663HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.National Aeronautics and Space Administration-$13.82K2009-04-161997-05-31ENVIROMENTAL TEST ARTICLE AND REGENERATIVE LIFE SUPPORT TEST PROGRAMS