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Valley Tech Systems, INC.

$46M obligated·31 awards·2 agencies·3 NAICS

Federal Contracts

Showing contracts 5163 of 63 total. Sorted by action date, most recent first. Excludes $0 modifications.

DateAgencyPIIDNAICSDescriptionAmount
Jun 5, 2018Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014718C7014541715SBIR/STTR PHASE II R&D - AFFORDABLE EXTINGUISHABLE DIVERT AND ATTITUDE CONTROL SYSTEMS (XDACS)$987K
Jun 5, 2018Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014717C7424541712IGF::OT::IGF SBIR/STTR PHASE II R&D$58K
Apr 27, 2018National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER80NSSC18C0149541715DUE TO THE RAPID MATURITY OF SMALL SATELLITE TECHNOLOGIES TO MEET NEAR TERM COMMERCIAL, SCIENCE AND MILITARY SPACE APPLICATIONS THERE IS A DRIVING NEED FOR DEVELOPMENT OF INCREASED AFFORDABLE SPACE LAUNCH SYSTEM CAPABILITY. TO ADDRESS THIS NEED, VALLEY TECH SYSTEMS IS PROPOSING A SBIR PHASE II DEVELOPMENT OF A NEW SOLID PROPULSION REACTION CONTROL SYSTEM (RCS) THAT LEVERAGES OVER 12 YEARS AND $12M OF PARALLEL MDA AND USAF CONTROLLABLE SOLID PROPULSION MISSILE INTERCEPTOR AND STRATEGIC DETERRENT PROPULSION TECHNOLOGY INVESTMENTS. THIS NEW TECHNOLOGY WILL REPLACE OLDER, HEAVIER AND LESS PREFORMING COLD GAS ACS PRODUCTS PROVIDING NASA AND FUTURE LAUNCH SYSTEM PROVIDERS WITH INCREASED CAPABILITY WITH IMPROVED AFFORDABILITY. OUR SOLID RCS IS APPLICABLE TO BOTH A FUTURE COMMERCIAL BOOSTER FLYOUT ATTITUDE CONTROL SYSTEM (ACS) APPLICATIONS AND FUTURE POST BOOST PROPULSION SYSTEM (PBPS) PAYLOAD DELTA-V AND ACS PROVIDING INCREASED SATELLITE ORBITAL INSERTION ACCURACIES. THE PHASE II PROGRAM WILL MATURE THE NEW SOLID RCS TECHNOLOGY TO A TRL-6 READY FOR INSERTION INTO FOLLOW-ON COMMERCIAL LAUNCH SYSTEM INTEGRATION AND FLIGHT TESTING. THE RESULT IS A NEW AFFORDABLE SOLID RCS THAT FILLS AN IDENTIFIED CRITICAL TECHNICAL GAP FOR FUTURE AFFORDABLE ACCESS TO SPACE.$750K
Feb 1, 2018Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7705541712::IGF::OT::IGF SBIR PHASE II RESEARCH&DEVELOPMENT$499K
Jun 19, 2017Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014717C7424541712IGF::OT::IGF SBIR/STTR PHASE II R&D$1000K
Jun 7, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CM64P541712IGF::OT::IGF DURING THIS PHASE I SBIR PROGRAM VALLEY TECH SYSTEMS, INC. (VTS) WILL DEVELOP NEW LONG DURATION SOLID PROPELLANT THRUST THROTTLING TECHNOLOGY FOR AN AFFORDABLE LAUNCH VEHICLE REACTION CONTROL SYSTEM (RCS) FOR SMALL SATELLITE ORBITAL INSERTION APPLICATIONS. THE NEW AFFORDABLE RCS PROPULSION TECHNOLOGY PROVIDES NASA WITH ACCURATE LAUNCH VEHICLE UPPER STAGE BOOSTER ATTITUDE CONTROL, POST BOOST SATELLITE DELTA-V AND ACCURATE ORBITAL INSERTION THRUST USING NON-TOXIC AND STORABLE SOLID PROPULSION. ADDITIONALLY, THE SOLID PROPULSION THROTTLING TECHNOLOGY FEATURES FLEXIBLE IMPULSE AND ACCURATE THRUST THROTTLING IN A MODULAR CONSTRUCTED ARCHITECTURE FOR EASE OF ADAPTING TO NUMEROUS FUTURE NASA LAUNCH VEHICLE APPLICATIONS. THE PHASE I PROGRAM WILL CONDUCT TOP LEVEL SYSTEM TRADES, DESIGN CONCEPT LAYOUTS AND CRITICAL TECHNOLOGY TESTING TO YIELD A SMOOTH AND CLEAR TRANSITION FROM THE PHASE I TO A PHASE II PROTOTYPE DEMONSTRATION PROGRAM.$125K
Aug 4, 2016Department of DefenseFA9300 AFTC PZRFA930015C2008541712IGF::OT::IGF PHASE II SBIR CONTRACT LIGHTWEIGHT DETACHABLE ROLL CONTROL SYSTEM$187K
Jun 12, 2016Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7555541712SBIR PHASE I RESEARCH AND DEVELOPMENT::IGF::OT::IGF$40K
Jun 9, 2016Department of DefenseFA9300 AFTC PZRFA930016C2002541712IGF::OT::IGF SBIR II - AFFORDABLE SOLID PROPELLANT POST BOOST PROPULSION (PBPS) FOR A FUTURE ICBM WEAPON SYSTEM$746K
Jun 9, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CM47P541712IGF::OT::IGF DURING THIS PHASE I NASA PROGRAM, VALLEY TECH SYSTEMS (VTS) WILL DEVELOP AN INNOVATIVE SOLID REACTION CONTROL SYSTEM (RCS) ARCHITECTURE CONCEPT DESIGN THAT CAN MANAGE PITCH, YAW AND ROLL FOR THE MAV AS IT ASCENDS, COMPLETES STAGE SEPARATION, AND PERFORMS FINAL MANEUVERS FOR LINKING WITH THE CARRIER SATELLITE. THE INNOVATIVE DESIGN WILL LEVERAGE OUR ADVANCED, LONG DURATION, EXTINGUISHABLE AND RE-IGNITABLE SOLID PROPULSION SYSTEM, COUPLED WITH CRITICAL HOT GAS VALVE AND PROPORTIONAL THRUSTER TECHNOLOGIES, TO PROVIDE AN OPTIMAL SOLID ROCKET MOTOR BASED CONTROL SYSTEM THAT ACTS LIKE A LIQUID SOLUTION. DUE TO THE INHERENT ABILITY OF SOLID PROPULSIVE CONTROL SYSTEMS TO ACCOMMODATE COLD SPACE ENVIRONMENTS, THE SYSTEM REQUIRES FEWER HEATERS, THEREFORE IMPROVING RELIABILITY. MOREOVER, SOLID CONTROL SYSTEMS HAVE THE ABILITY TO MEET A HIGHER RANGE OF THRUST WITH THE SAME THRUSTER SET TO MINIMIZE INERT WEIGHT AND IMPROVE VEHICLE CONTROLLABILITY. THE PHASE I PROGRAM WILL CONDUCT TOP LEVEL SYSTEM TRADES, DESIGN CONCEPT LAYOUTS, AND PERFORM CRITICAL TECHNOLOGY TESTING TO YIELD A SMOOTH AND CLEAR TRANSITION FROM THE PHASE I TO A PHASE II PROTOTYPE DEMONSTRATION PROGRAM.$124K
May 6, 2016Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7706541712IGF::OT::IGF 7706 PHASE II RESEARCH&DEVELOPMENT$1000K
Mar 8, 2016Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7705541712::IGF::OT::IGF SBIR PHASE II RESEARCH&DEVELOPMENT$1000K
Dec 17, 2015Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7555541712SBIR PHASE I RESEARCH AND DEVELOPMENT::IGF::OT::IGF$100K

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