Federal Contractor Profile
Tda Research, INC.
$143M obligated·292 awards·7 agencies·8 NAICS
Federal Contracts
Showing contracts 251–300 of 348 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Feb 7, 2019 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N0017818C8009 | 541715 | BASE | $500K |
| Oct 3, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833519C0067 | 541715 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $125K |
| Sep 28, 2018 | Department of DefenseNSWC INDIAN HEAD DIVISION | N0017418C0025 | 541715 | SBIR PHASE I TOPIC - CONDUCTIVE PROPELLANT ADDITIVES FOR ELECTRICAL IGNITION | $150K |
| Sep 27, 2018 | Department of DefenseFA8051 772 ESS PKD | FA805118P0020 | 541715 | SBIR PHASE I NON-FLUORINATED AFFF REPLACEMENT | $150K |
| Sep 20, 2018 | Department of DefenseCOMMANDER | M6785418C6514 | 541715 | IGF::OT::IGF - RESEARCH AND DEVELOPMENT | $496K |
| Sep 19, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C5018 | 541715 | SBIR II LOW HYDROGEN EMBRITTLEMENT BRUSH PLATING CHEMISTRIES | $750K |
| Sep 18, 2018 | Department of DefenseW6QK ACC-APG | W91CRB18C0029 | 541715 | BASE YEAR (12 MONTHS) | $1.2M |
| Sep 17, 2018 | Department of DefenseW4GG HQ US ARMY TACOM | W56HZV18C0162 | 541715 | FY 2017 BAA FOR MULTI-FUEL REFORMER FOR BATTLEFIELD HYDROGEN. | $998K |
| Sep 10, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0756 | 541715 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $125K |
| Sep 7, 2018 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND14PC00067 | 541712 | IGF::OT::IGF HELMET-MOUNTED THERMAL SENSOR FOR FIRST RESPONDER BURN-SAVER DEVICE | $1K |
| Aug 20, 2018 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH18C0110 | 541715 | DHA 17.1 SBIR PHASE II MEDICAL R&D CONTRACT FOR PROPOSAL #H2-0356, TITLED: "INTELLIGENT THERMAL DESORPTION TUBE SEQUENTIAL SAMPLER" ERMS18116003 | $1.0M |
| Aug 20, 2018 | Department of DefenseW6QK ACC-APG DURHAM | W911NF18C0062 | 541715 | STTR PHASE II | $1000K |
| Jul 26, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1939 | 541715 | HUMAN EXPLORATION OF MARS, AS WELL AS UNMANNED SAMPLE RETURN MISSIONS FROM MARS CAN BENEFIT GREATLY FROM THE USE OF PROPELLANTS AND LIFE-SUPPORT CONSUMABLES PRODUCED FROM THE RESOURCES AVAILABLE ON MARS MARS CO2 RICH ATMOSPHERE OFFERS AN ABUNDANT STARING MATERIAL ON WHICH TO SYNTHESIZE NEEDED RESOURCES SUCH AS OXYGEN, CARBON MONOXIDE, AND METHANE. THE PREFERRED METHOD OF OXYGEN GENERATION USES A SOLID OXIDE ELECTROLYZER (SOE) TO PRODUCE OXYGEN IN ONE STREAM AND A MIXTURE OF CARBON MONOXIDE AND CARBON DIOXIDE AS THE WASTE GASES. TDA RESEARCH PROPOSES TO DEVELOP A HIGHLY EFFICIENT SYSTEM FOR SEPARATION AND RE-CIRCULATION OF THE UNREACTED CO2 FROM THE SOE PROCESSES. TDA S SYSTEM USES A NOVEL ADSORBENT THAT REMOVES THE UNREACTED CO2 AT TEMPERATURES>650 C, WITHOUT ANY NEED FOR COOLING IT DOWN. THE SPECIFIC OBJECTIVE OF THE PHASE I WORK IS TO DEVELOP A REGENERABLE HIGH TEMPERATURE CO2 SORBENT THAT REGENERATES VIA THERMAL SWING OR PRESSURE (VACUUM) SWING AND DEMONSTRATE THE EJECTOR CONCEPT AND THERMAL SWING CONCEPT FOR GAS RECIRCULATION IN A BREADBOARD SYSTEM. | $125K |
| Jul 26, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1903 | 541715 | HYPERSONIC AIRCRAFT, ESPECIALLY REUSABLE HYPERSONIC AIRCRAFT, REQUIRE ADVANCEMENTS IN HIGH TEMPERATURE MATERIALS BECAUSE OF THE EXTREME TEMPERATURES RESULTING FROM FRICTIONAL HEATING. ONE ASPECT OF THIS PROBLEM IS MAKING SEALS THAT CAN FUNCTION THROUGH A VERY LARGE TEMPERATURE RANGE, PERHAPS UP TO 1000 C OR HIGHER. METALLIC SPRINGS ESSENTIALLY LOSE THEIR ABILITY TO FUNCTION AT 600 C OR BELOW. CERAMIC SPRINGS, PRINCIPALLY MADE OF SILICON NITRIDE, ARE CAPABLE OF FUNCTIONING THROUGHOUT THAT TEMPERATURE RANGE, BUT LACK THE STRENGTH REQUIRED FOR MOST APPLICATIONS. THEY ALSO UNDERGO VERY LIMITED DEFORMATION BEFORE FAILURE. TDA WILL IMPROVE THE FEEDSTOCKS AND MODIFY THE EXISTING PROCESS FOR MANUFACTURING CERAMIC COMPRESSION SPRINGS. THROUGH IMPROVEMENTS TO THE GRAIN STRUCTURE, THE RESULTING SPRINGS WILL OVERCOME THEIR PREVIOUS LIMITATIONS. | $125K |
| Jul 25, 2018 | Department of DefenseCOMMANDER | M6785416C6504 | 541711 | SBIR PHASE II RESEARCH AND DEVELOPMENT IGF::OT::IGF FOR OTHER FUNCTIONS | $250K |
| Jul 23, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N0002417P4509 | 541712 | STATUS REPORT IGF::OT::IGF | $70K |
| Jul 18, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0177 | 541715 | TDA RESEARCH INC.(TDA) IN COLLABORATION WITH UNIVERSITY OF PUERTO RICO MAYAGUEZ (UPRM IS PROPOSING TO DEVELOP A HIGHLY EFFICIENT CO2 REMOVAL SYSTEM BASED ON UPRM PROPRIETARY STRONTIUM EXCHANGED SILICO-ALUMINO-PHOSPHATE (SR-SAPO-34) SORBENT FOR CLOSED LOOP SPACE CRAFT CABIN AIR RE-VITALIZATION DURING DEEP SPACE MISSIONS. IN THE PHASE I WORK, WE SUCCESSFULLY COMPLETED BENCH-SCALE PROOF-OF-CONCEPT DEMONSTRATIONS, ELEVATING THE TRL TO 3. IN PHASE II, WE WILL FURTHER OPTIMIZE THE SORBENT AND SCALE-UP ITS PRODUCTION USING ADVANCED MANUFACTURING TECHNIQUES SUCH AS CONTINUOUS MICROWAVE SYNTHESIS. WE WILL CARRY OUT MULTIPLE ADSORPTION/DESORPTION CYCLES TO DEMONSTRATE THE SORBENT'S CYCLE LIFE (>500). WE WILL DEVELOP A CFD MODEL TO OPTIMIZE THE CYCLIC OPERATION OF THE SORBENT SYSTEM AND CARRY OUT A DETAILED ENGINEERING ASSESSMENT OF THE FULL-SCALE SYSTEM. FINALLY, WE WILL DESIGN AND FABRICATE A SUB-SCALE PROTOTYPE TO FULLY DEMONSTRATE THE TECHNOLOGY UNDER SIMULATED SPACECRAFT CABIN ATMOSPHERES (TRL-5); THIS UNIT WILL BE SENT TO NASA FOR FURTHER TESTING AND EVALUATION. | $750K |
| Jul 11, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2504 | 541715 | THIS STATEMENT OF WORK (SOW) ADDRESSES MATERIAL SUPPLY REQUEST FOR THE US INTERNATIONAL SPACE STATION (ISS) AMMONIA SCRUBBER. THE INTENT OF THIS STATEMENT OF WORK IS TO OUTLINE ACTIVITIES AND DELIVERABLES TO SUPPORT DELIVERY OF CLASS I FLIGHT GRADE SORBENT MEDIA TO SUPPORT A NOVEMBER 2018 FLIGHT DATE. THE AMMONIA SCRUBBER IS DESIGNED TO REMOVE AMMONIA FROM THE CABIN OF THE COMMERCIAL CREW VEHICLES DURING AN AMMONIA LEAK ON THE INTERNATIONAL SPACE STATION. TDA DEVELOPED A SORBENT MEDIA DESIGNED TO BE PACKED INTO AN AMMONIA SCRUBBER BED THIS SOW IS A SBIR PHASE III REFERENCING SBIR PHASE 2 PROJECT NNX15CJ07C (H3.02-9398) AN ADVANCED SMOKE-EATER FOR POST FIRE CABIN ATMOSPHERE CLEANUP. | $269K |
| Jun 28, 2018 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND14PC00067 | 541712 | IGF::OT::IGF HELMET-MOUNTED THERMAL SENSOR FOR FIRST RESPONDER BURN-SAVER DEVICE | $17K |
| Jun 26, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018C5016 | 541715 | CORROSION INDICATING COATINGS FOR AIRCRAFT BILGES AND WHEEL WELLS | $750K |
| Jun 13, 2018 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH18C0121 | 541715 | DHA PHASE I SBIR PROPOSAL H181-003-0064 | $150K |
| Jun 12, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0632 | 541715 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $125K |
| Jun 12, 2018 | Department of DefenseHQ USSOCOM | H9240518P0006 | 541715 | IGF::OT::IGF FEASIBILITY STUDY, SBIR PHASE I, TOPIC SOCOM181- 003, TACTICAL ACTIVE ANTI-FOGGING GOGGLE OR SPECTACLE | $150K |
| Jun 11, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0494 | 541715 | PROGRESS REPORT | $125K |
| Jun 7, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833517C0202 | 541712 | RESEARCH AND DEVELOPMENT, SBIR PHASE II, IGF::OT::IGF | $374K |
| Jun 4, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0578 | 541715 | RESEARCH AND DEVELOPMENT IGF::OT::IGF | $125K |
| May 10, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0136 | 541715 | SOLID-CORE NUCLEAR THERMAL PROPULSION (NTP) HAS BEEN IDENTIFIED AS THE ADVANCED PROPULSION CONCEPT WHICH COULD PROVIDE THE FASTEST TRIP TIMES WITH FEWER SPACE LAUNCH SYSTEM (SLS) LAUNCHES FOR HUMAN MISSIONS TO MARS. CURRENT ENVIRONMENTAL REGULATIONS REQUIRE THAT RADIOACTIVE HALOGENS, NOBLE GASES, AEROSOLS AND PARTICULATES MUST BE FILTERED OUT OF NTP ENGINE EXHAUST DURING GROUND TESTING. IN PHASE I, WE DEMONSTRATED THE ABILITY OF OUR SORBENT TO REMOVE PPM LEVELS OF HALOGENS AND NOBLE GASES FROM HELIUM AT HIGH SPACE VELOCITIES OVER MULTIPLE REGENERATION CYCLES. IN THIS SBIR PHASE II PROJECT, TDA RESEARCH, INC. PROPOSES TO DEVELOP A NOVEL SCRUBBER THAT CONTAINS OUR HIGH-CAPACITY SORBENT TO REMOVE OF THE RADIOACTIVE HALOGENS AND NOBLE GASES FROM NTP ENGINE EXHAUST, AS PART OF NASA'S LARGER EXHAUST TREATMENT SYSTEM. IN PHASE II, WE WILL CONTINUE TO OPTIMIZE THE SORBENT FORMULATION, SCALE UP ITS PRODUCTION, AND DESIGN AND BUILD A PORTABLE SUB-SCALE UNIT TO DEMONSTRATE ITS ABILITY TO SELECTIVELY REMOVE>99.5% RADIOACTIVE HALOGENS AND NOBLE GASES UNDER SIMULATED NTP ENGINE EXHAUST CONDITIONS. BASED ON THE PERFORMANCE RESULTS, WE WILL CARRY OUT A DETAILED DESIGN OF THE FULL-SIZE SCRUBBING SYSTEM FOR TREATING NTP ENGINE EXHAUST AND ESTIMATE ITS SIZE, COST AND ENERGY REQUIREMENTS. | $750K |
| May 10, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18C0135 | 541715 | HUMAN EXPLORATION OF MARS AND UNMANNED SAMPLE RETURN MISSIONS CAN BENEFIT GREATLY FROM THE RESOURCES AVAILABLE ON MARS. THE FIRST MAJOR STEP OF ANY MARS IN-SITU PROPELLANT PRODUCTION SYSTEM IS THE ACQUISITION OF CARBON DIOXIDE AND ITS COMPRESSION FOR FURTHER PROCESSING. TDA RESEARCH INC. PROPOSES TO DEVELOP A COMPACT, LIGHTWEIGHT, ADVANCED SORBENT-BASED COMPRESSOR TO RECOVER HIGH-PRESSURE, HIGH PURITY CO2 FROM THE MARTIAN ATMOSPHERE. THE SYSTEM ELIMINATES THE NEED FOR A MECHANICAL PUMP, INCREASING THE RELIABILITY WITH RELATIVELY LOW POWER CONSUMPTION. TDA S SYSTEM USES A NEW, HIGH CAPACITY SORBENT THAT SELECTIVELY ADSORBS CO2 AT 0.1 PSIA AND REGENERATES BY TEMPERATURE SWING, PRODUCING A CONTINUOUS, HIGH PURITY CO2 FLOW AT PRESSURE (>15 PSIA). IN THE PHASE I WORK, WE SUCCESSFULLY COMPLETED BENCH-SCALE PROOF-OF-CONCEPT DEMONSTRATIONS, ELEVATING THE TRL TO 3. IN PHASE II, WE WILL FURTHER OPTIMIZE THE SORBENT AND SCALE-UP ITS PRODUCTION USING ADVANCED MANUFACTURING TECHNIQUES SUCH AS CONTINUOUS MICROWAVE SYNTHESIS. WE WILL CARRY OUT MULTIPLE ADSORPTION/DESORPTION CYCLES TO DEMONSTRATE THE SORBENT'S CYCLE LIFE. FINALLY, WE WILL DESIGN AND FABRICATE A SUB-SCALE PROTOTYPE TO FULLY DEMONSTRATE THE TECHNOLOGY UNDER SIMULATED MARTIAN ATMOSPHERES (TRL-5); THIS UNIT WILL BE SENT TO NASA FOR FURTHER TESTING AND EVALUATION. | $750K |
| Apr 25, 2018 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865018P2004 | 541715 | EXHAUST GAS TEMPERATURE SENSING USING THERMALLY LUMINESCENT COMPOUNDS | $150K |
| Apr 3, 2018 | Department of Homeland SecuritySCI TECH ACQ DIV | 70RSAT18C00000008 | 541715 | IGF::OT::IGF DEPARTMENT OF HOMELAND SECURITY, SCIENCE AND TECHNOLOGY, FY17.1 PHASE II CONTRACT PROPOSAL TITLE: WEARABLE SMART CHEMICAL SENSORS | $750K |
| Mar 27, 2018 | Department of DefenseDEFENSE THREAT REDUCTION AGENCY | HDTRA118P0015 | 541715 | T172-001-0098 SBIR PHASE I FOR CONSTRUCTION OF LARGE N ACOUSTIC ARRAY | $150K |
| Mar 13, 2018 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH18C0019 | 541715 | DHA SBIR PHASE I - H172-011-0152 | $150K |
| Feb 27, 2018 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C0042 | 541712 | ALUMINUM ALLOY CORROSION CONTROL AND PREVENTION | $519K |
| Jan 16, 2018 | Department of DefenseNSWC DAHLGREN | N0017818C8009 | 541715 | BASE | $500K |
| Dec 13, 2017 | Department of the InteriorIBC ACQ SERVICES DIVISION (00063) | IND14PC00067 | 541712 | IGF::OT::IGF HELMET-MOUNTED THERMAL SENSOR FOR FIRST RESPONDER BURN-SAVER DEVICE | $250K |
| Sep 28, 2017 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ17HD06P | 541712 | IGF::OT::IGF TDA SBIR PHASE III IMPROVED MATERIALS AND HARDWARE FOR TRACE CONTAMINANT CONTROL | $45K |
| Sep 25, 2017 | Department of DefenseCOMMANDER | M6785417P6525 | 541712 | IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT | $70K |
| Sep 22, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0213 | 541712 | IGF::OT::IGF DHA SBIR PHASE II AWARD | $1000K |
| Sep 20, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0141 | 541712 | IGF::OT::IGF DHA SBIR PHASE II PROPOSAL A2-6698 | $1000K |
| Sep 20, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0210 | 541712 | IGF::OT::IGF DHA SBIR PHASE II AWARD | $1000K |
| Sep 18, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0081 | 921190 | IGF::OT::IGF DHP SBIR PHASE II PROPOSAL H2-0195 | $1000K |
| Sep 8, 2017 | Department of DefenseW4PZ USA MED RSCH ACQUIS ACT | W81XWH17C0136 | 541712 | IGF::OT::IGF DHP PHASE I PROPOSAL H171-006-0104 TOPIC DHA17-006 INTELLIGENT THERMAL DESORPTION TUBE SEQUENTIAL SAMPLER ERMS 17100002 | $150K |
| Aug 16, 2017 | Environmental Protection AgencyRTP PROC OPS DIVISION (RTPPOD) | EPD17038 | 541712 | IGF::OT::IGF SBIR PHASE I: TDA RESEARCH, INC. | $100K |
| Aug 16, 2017 | Department of DefenseOFFICE OF NAVAL RESEARCH | N0001415C0042 | 541712 | ALUMINUM ALLOY CORROSION CONTROL AND PREVENTION | $1.0M |
| Aug 15, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017C5071 | 541712 | IGF::OT::IGF SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II CHROMATE-FREE FLEXIBLE COATING | $750K |
| Aug 4, 2017 | Department of DefenseW6QK ACC-APG | W91CRB16C0023 | 541712 | VECTOR PROTECTION - DETERMINATION OF ACTIVE INGREDIENT LEVELS FOR A NEW PYRETHROID UNIFORM TREATMENT FORMULATION | $395K |
| Jun 22, 2017 | Department of DefenseW6QK ACC-APG DURHAM | W911NF13C0096 | 541712 | IGF::OT::IGF FIRST MONTHLY PROGRESS REPORT | $15K |
| Jun 16, 2017 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865017P5051 | 541711 | IGF::OT::IGF BRUSH-PLATED LOW HYDROGEN EMBRITTLEMENT TIN-ZINC ALLOY COATING FOR THE REPLACEMENT OF CADMIUM | $150K |
| Jun 14, 2017 | National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER | NNJ17HD06P | 541712 | IGF::OT::IGF TDA SBIR PHASE III IMPROVED MATERIALS AND HARDWARE FOR TRACE CONTAMINANT CONTROL | $122K |
| Jun 9, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CS17P | 541712 | IGF::OT::IGF SOLID CORE NUCLEAR THERMAL PROPULSION (NTP) HAS BEEN IDENTIFIED AS THE ADVANCED PROPULSION CONCEPT WHICH COULD PROVIDE THE FASTEST TRIP TIMES WITH FEWER SPACE LAUNCH SYSTEM (SLS) LAUNCHES FOR HUMAN MISSIONS TO MARS. HOWEVER, CURRENT ENVIRONMENTAL REGULATIONS REQUIRE NTP ENGINE EXHAUST FILTERING OF RADIOACTIVE HALOGENS, NOBLE GASES AND PARTICULATES TO STAY WITHIN SAFE LIMITS. PARTICULARLY HIGH EFFICIENCY (GREATER THAN 99.5%) REMOVAL OF RADIOACTIVE HALOGENS, NOBLE GASES AND VAPOR PHASE CONTAMINANTS IS OF SPECIFIC INTEREST TO NASA. IN THIS SBIR PROJECT, TDA RESEARCH, INC. PROPOSES TO DEVELOP A NOVEL HIGH CAPACITY SORBENT TO REMOVE RADIOACTIVE HALOGENS AND NOBLE GASES FROM NTP ENGINE EXHAUST WITH AN EFFICIENCY GREATER THAN 99.5%. THIS SORBENT WILL BE PART OF AN EFFLUENT SCRUBBER SYSTEM, WHICH INITIALLY COOLS THE HOT HYDROGEN EXHAUST WITH A WATER SPRAY, AND THEN FURTHER COOLS IT AND REMOVES THE WATER IN A SERIES OF HEAT EXCHANGERS. IN PHASE I, WE WILL PREPARE THE SORBENT AND DEMONSTRATE ITS ABILITY TO SELECTIVELY REMOVE RADIOACTIVE HALOGENS AND NOBLE GASES UNDER SIMULATED NTP ENGINE EXHAUST CONDITIONS. BASED ON THE PERFORMANCE RESULTS, WE WILL CARRY OUT A PRELIMINARY DESIGN OF THE SCRUBBING SYSTEM FOR NTP ENGINE EXHAUST AND ESTIMATE ITS SIZE AND COST. | $125K |
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