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Tda Research, INC.

$143M obligated·292 awards·7 agencies·8 NAICS
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Federal Contracts

Showing contracts 301–348 of 348 total. Sorted by action date, most recent first. Excludes $0 modifications.

DateAgencyPIIDNAICSDescriptionAmount
Jun 6, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CM55P541712IGF::OT::IGF AN ADVANCED ENVIRONMENTAL CONTROL AND LIFE SUPPORT SYSTEM (ECLSS) FOR LONG DURATION MANNED SPACE MISSIONS ?SUCH AS PLANETARY FLIGHT MISSIONS OR PLANETARY BASES- REQUIRES AN ALMOST COMPLETE CLOSURE OF ALL RELEVANT MATERIAL LOOPS. ENERGY EFFICIENT CARBON DIOXIDE (CO2) REMOVAL AND REDUCTION SYSTEMS ARE CRITICAL TO REDUCING THE POWER CONSUMPTION OF THE SPACECRAFT ATMOSPHERE REVITALIZATION SYSTEMS. TDA PROPOSES TO DEVELOP A RAPIDLY CYCLING VACUUM-ASSISTED THERMAL SWING ADSORPTION (VTSA) SYSTEM TO REMOVE CO2 FROM CABIN AIR AND CONCENTRATE IT FOR SUBSEQUENT REDUCTION AND PRESSURIZATION. OUR UNIQUE SORBENT EXHIBITS ONE OF THE HIGHEST CAPACITIES REPORTED FOR CO2 ADSORPTION AT VERY LOW CO2 PARTIAL PRESSURES (1-3 TORR CO2 PARTIAL PRESSURE RANGE). THE LOW HEAT OF ADSORPTION OF CO2 ON THE SORBENT AND THE RELATIVELY LOW HEAT INPUT NEEDED TO DESORB THE CO2 ACROSS A SMALL TEMPERATURE DIFFERENTIAL DURING REGENERATION WILL REDUCE THE POWER REQUIREMENT FOR THE PROCESS. THE NEW MATERIAL IS ALSO HIGHLY TOLERANT TO MOISTURE. IN PHASE I, WE WILL PREPARE THE SORBENT AND DEMONSTRATE ITS ABILITY IN SELECTIVELY REMOVING CO2 FROM AIR UNDER REPRESENTATIVE CONDITIONS. THE TECHNOLOGY READINESS LEVEL (TRL) WILL BE ELEVATED TO 3 AT THE END OF PHASE I. WE WILL ALSO COMPLETE THE DETAILED DESIGN OF THE VTSA REACTOR. IN PHASE II, WE WILL BUILD A HIGH FIDELITY PROTOTYPE ASSEMBLY AND DEMONSTRATE THE CONCEPT AT FULL-SCALE, ELEVATING THE TRL TO 5.$125K
Jun 6, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CC81P541712IGF::OT::IGF 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.$125K
Jun 5, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CP69P541712IGF::OT::IGF A LANDER ON THE SURFACE OF VENUS IS HEATED BY THE 460 C SURFACE TEMPERATURE, WHICH, EVEN WITH THE BEST CURRENT DESIGNS USING PASSIVE INSULATION, CAUSE ITS ELECTRONICS TO FAIL IN MUCH LESS THAN A DAY. ACTIVE COOLING CONCEPTS ARE NOT ONLY EXCEEDINGLY HEAVY BUT ALSO EXCEEDINGLY INEFFICIENT. TDA PROPOSES A NEW INSULATION FOR THE EXTERIOR OF THE LANDER THAT INCORPORATES HEAT REJECTION MECHANISMS THAT APPARENTLY HAVE NOT BEEN PREVIOUSLY CONSIDERED FOR THE VENUS SURFACE. OUR INSULATION WILL MAKE USE OF A FLEXIBLE MATERIAL THAT HAS BEEN RECENTLY DEVELOPED AT TDA, AND WE WILL COMPARE IT TO OTHER POTENTIAL BUT BRITTLE INSULATIONS. ORDER-OF-MAGNITUDE CALCULATIONS SUGGEST THAT THE LIFETIME OF THE LANDER CAN BE EXTENDED FROM HOURS TO DAYS.$125K
Jun 1, 2017National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX17CS16P541712IGF::OT::IGF NASA USES AN ESTIMATED 75 MILLION STANDARD CUBIC FEET OF HELIUM (APPROXIMATELY $5M WORTH) EACH YEAR FOR SAFELY PURGING HYDROGEN SYSTEMS BEFORE FILLING AND AFTER DISCHARGING, AND WHILE LEAK CHECKING, PRESSURIZING LINES AND BLANKETING LIQUID HYDROGEN STORAGE TANKS. DESPITE ITS EXPENSE, THERE IS NO SUBSTITUTE FOR HELIUM IN MOST OF THESE APPLICATIONS BECAUSE OF ITS EXTREMELY LOW BOILING POINT AND UNIQUE CHEMICAL INERTNESS. THE PRICE OF HELIUM IS EXPECTED TO INCREASE AS RESERVES ARE DRAWN DOWN. IN ADDITION TO HELIUM, THE HIGH SUPPLY COSTS AND LIMITED AVAILABILITY OF HYDROGEN FUEL ALSO REQUIRES ITS CONSERVATION. WHILE IT IS NOT AS EXPENSIVE AS HELIUM AND IS MORE ABUNDANT, THE TRANSPORT OF HYDROGEN IS STILL COSTLY AND POSES A GREAT ENVIRONMENTAL RISK DUE ITS FLAMMABILITY AND HIGHLY REACTIVE NATURE. THEREFORE, AN EFFICIENT WAY TO SEPARATE THE HE/H2 FROM NASA?S PURGE STREAMS AND RECOVER BOTH THE HELIUM AND HYDROGEN IN A PURE FORM IS CRITICAL TO REDUCE COST OF OPERATIONS AND TO REDUCE RISKS. IN PHASE I WE WILL SYNTHESIZE AND OPTIMIZE A NEW SORBENT AND DEVELOP A PROCESS AND CYCLE SCHEME THAT WILL ALLOW US TO ACHIEVE THE TARGET HELIUM AND HYDROGEN PURITIES WITH LOW ENERGY CONSUMPTION.$125K
May 31, 2017Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865017P5047541711IGF::OT::IGF CORROSION INDICATING COATINGS FOR AIRCRAFT BILGES$150K
May 1, 2017Department of DefenseNSWC DAHLGRENN0002416P4090541712STATUS REPORT IGF::OT::IGF$70K
Apr 27, 2017Department of Homeland SecuritySCI TECH ACQ DIVHSHQDC17C00031541712IGF::OT::IGF DEPARTMENT OF HOMELAND SECURITY, SCIENCE AND TECHNOLOGY. FY17.1 PHASE I CONTRACT PROPOSAL TITLE: WEARABLE CHEMICAL SENSOR BADGE$100K
Mar 29, 2017Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833517C0090541712IGF::OT::IGF RESEARCH AND DEVELOPMENT$396K
Mar 13, 2017Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833517C0202541712RESEARCH AND DEVELOPMENT, SBIR PHASE II, IGF::OT::IGF$375K
Mar 2, 2017Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH17C0001541712IGF::OT::IGF PROPOSAL A161-049-0713$100K
Feb 24, 2017Environmental Protection AgencyRTP PROC OPS DIVISION (RTPPOD)EPD17025541712IGF::OT::IGF FUND 2017 SBIR PHASE II NEW AWARD- TDA RESEARCH, INC. - ISOCYANATE-FREE POLYURETHANE COATING$300K
Dec 30, 2016Department of DefenseCOMMANDERM6785417P6525541712IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT$80K
Nov 15, 2016Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014717C7316541712SBIR PHASE II RESEARCH&DEVELOPMENT;;IGF::OT::IGF$999K
Oct 24, 2016Department of DefenseNAVSEA HQN0002417P4509541712STATUS REPORT IGF::OT::IGF$80K
Sep 8, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH16C0088541712IGF::OT::IGF-DHP PHASE I PROPOSAL #H161-007-0088$150K
Sep 1, 2016Department of DefenseW6QK ACC-PICAW15QKN16C0064541712IGF::OT::IGF LOW-COST RAPID STAND-OFF DETECTION OF EXPLOSIVES SBIR PHASE I.$100K
Aug 25, 2016Department of DefenseCOMMANDERM6785416C6504541711SBIR PHASE II RESEARCH AND DEVELOPMENT IGF::OT::IGF FOR OTHER FUNCTIONS$500K
Aug 16, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH16C0054541712IGF::OT::IGF DHP SBIR 16.1 PH I AWARD$150K
Aug 12, 2016Department of DefenseNAVSEA HQN0002416P4090541712STATUS REPORT IGF::OT::IGF$80K
Aug 2, 2016Department of DefenseW6QK ACC-APG NATICKW911QY16P0300541712FINAL TECHNICAL REPORT BASE PERIOD IGF::OT::IGF$100K
Aug 2, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH16C0073541712IGF::OT::IGF. DHP PHASE II PROPOSAL H2-0175 ENTITLED, "OPTIMAL REWARMING SOLUTIONS FOR CRYOPRESERVED TISSUE SYSTEMS".$1000K
Aug 1, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH16C0076921190IGF::OT::IGF SBIR PHASE I DHP H161-010-0107$150K
Jul 12, 2016Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0044541712SBIR PI R&D. IGF::OT::IGF$70K
Jul 11, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001416P1031541712STTRSOL2016.A IGF::CT::IGF$80K
Jul 7, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001416P3036541712IGF::CT::IGF SBIRSOL2016.1$80K
Jul 6, 2016Department of DefenseDCSO PHILADELPHIASP470116M0096541611IGF::OT::IGF!8503401330!SERVICES - MANAG$100K
Jun 28, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865016M5064541711IGF::OT::IGF PHASE I SBIR "CHROMATE-FREE FLEXIBLE PRIMER"$150K
Jun 20, 2016National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTERNNJ16HD66P541712IGF::OT::IGF SBIR PHASE III CONTRACT WITH TDA RESEARCH DESIGN, MANUFACTURE, TEST, AND PERFORMANCE REPORTING OF A WATER SAVE SYSTEM THAT FITS IN A SINGLE LOCKER$150K
Jun 16, 2016Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7527541712IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT$40K
Jun 9, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CA28P541712IGF::OT::IGF TDA RESEARCH IS PROPOSING TO CHEMICALLY MODIFY THE POLYMER BACKBONE OF POLYMERS KNOWN TO HAVE CHAR YIELDS UPWARDS OF 70% AT 800+ C (UNDER INERT GAS) IN ORDER TO MAKE THE POLYMERS FLEXIBLE, AND POSSIBLY ELASTOMERIC AT OR NEAR ROOM TEMPERATURE. FLEXIBILITY IS A RESULT OF EASY ROTATION AROUND THE BONDS WITHIN A POLYMER BACKBONE, MAINTAINED ONLY IN THE PRESENCE OF LOW CROSSLINK DENSITY. CONVERSELY, A HIGH CHAR YIELD REQUIRES VERY ROBUST BONDING, GENERALLY WITH HIGH CROSSLINK DENSITY, SINCE FLOPPY, EASILY BROKEN BONDS LEAD TO THE EVOLUTION OF GAS, REDUCING THE RESIDUAL MASS. OUR MODIFICATIONS WILL REDUCE THE CHAR YIELD, BUT, IN THIS CASE, EVEN A 10% LOSS IN CHAR YIELD WOULD STILL BE COMPARABLE TO THE CHAR YIELD OF THE INFLEXIBLE PHENOLIC RESINS CURRENTLY IN USE.$125K
Jun 8, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CA52P541712IGF::OT::IGF 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) FOR CLOSED LOOP SPACE CRAFT CABIN AIR RE-VITALIZATION DURING DEEP SPACE MISSIONS.$125K
May 26, 2016Department of DefenseW6QK AATD CONTR OFFW911W615C0009541712IGF::OT::IGF PAINT ADDITVE FOR EARLY DECTECTION OF CORROSION ~ SBIR PHASE II$550K
May 26, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865015C5093541712IGF::OT::IGF SBIR II TDA RESEARCH, INC.$187K
May 23, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CJ27P541712IGF::OT::IGF ACCORDING TO NASA, IT COSTS $10,000 TO MOVE A POUND OF MATERIAL FROM EARTH INTO ORBIT, AND 10 TO 40 TIMES MORE TO MOVIE TO THE MOON AND MARS. INSTEAD OF PAYING TO MOVE EACH SPARE PART, STRUCTURE SUPPORT, RADIATION SHIELD AND UTENSIL (ALONG WITH A WIDE RANGE OF OTHER PRODUCTS) FROM EARTH TO MARS EXTRATERRESTRIAL IN-SITU RESOURCES (SUNLIGHT, CO2 AND H2O) CAN BE CONVERTED INTO POLYETHYLENE. A WIDE RANGE OF PRODUCTS INCLUDING WATER BOTTLES, THIN FILMS, BAGS, HIGH PRESSURE PIPE AND AT ALMOST ANY SHAPE COULD BE PRODUCED USING ADDITIVE MANUFACTURING. POLYETHYLENE IS ALSO A CANDIDATE FOR RADIATION SHIELDING DUE TO ITS HIGH HYDROGEN CONTENT. TDA RESEARCH, INC. (TDA) PROPOSES TO DEVELOP A PLASTICS MANUFACTURING PLANT VIA IN SITU RESOURCE UTILIZATION. THE PLANT CONSISTS OF (1) A SOLAR POWERED GAS GENERATION SYSTEM TO PRODUCE CO AND H2 FROM INDIGENOUS CO2 AND H2O, (2) A MICRO-CHANNEL OLEFIN SYNTHESIS REACTOR THAT CONVERTS THE SYNTHESIS GAS (CO AND H2) TO LIGHT OLEFINS, (3) A POLYETHYLENE SYNTHESIS REACTOR, (4) A REFORMER FOR PROCESSING UNREACTED GASES AND BY-PRODUCTS BACK INTO MORE SYNTHESIS GAS FEEDSTOCK. IN PHASE I, WE WILL FOCUS ON DEMONSTRATING THE VIABILITY OF TWO OF THE KEY SUB-SYSTEMS: (1) TESTING A PROPRIETARY TDA CATALYST IN A MICRO-CHANNEL SYNGAS-TO-OLEFINS REACTOR AT SMALL SCALE, AND (2) REFINING A SMALL SCALE POLYETHYLENE SYNTHESIS SYSTEM THAT CONVERTS THE RANGE OF PRODUCTS FROM THE OLEFIN SYNTHESIS PROCESS INTO POLYETHYLENE AND OTHER CO-POLYMERS. WE WILL DESIGN A 5 KG/DAY POLYETHYLENE PRODUCTION PLANT, USING LAB DATA AND PERFORMANCE SPECIFICATIONS PROVIDED FOR EXISTING SYSTEMS SUCH AS THE ELECTRO-CHEMICAL CO2 REDUCTION TO CO, HYDROLYSIS FOR CONVERSION OF H2O TO H2, AND REFORMER TECHNOLOGY FOR CONVERTING UNREACTED GASES BACK TO SYNTHESIS GAS. PHASE I WILL PRODUCE A DETAILED DESIGN OF THIS SYSTEM, INCLUDING AN ESTIMATE OF THE WEIGHT AND VOLUME.$125K
May 23, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CJ53P541712IGF::OT::IGF A RECENT TRADE STUDY SHOWED THAT ACTIVE REMOVAL OF AMMONIA (NH3) AND FORMALDEHYDE (CH2O) IS CRTICIAL TO MEETING THE 24-HR SMAC LIMITS IN THE ADVANCED SPACE SUIT DESIGNS (JENNINGS 2009). TDA RESEARCH, INC. (TDA) PROPOSES TO DEVELOP A NEW TCCS FOR THE PLSS BASED ON A COMBINATION OF A REGENERABLE NH3 SORBENT AND AN AMBIENT TEMPERATURE CATALYST THAT CAN OXIDIZE FORMALDEHYDE INTO MUCH MORE BENIGN CO2 TO CONTROL THE CONCENTRATION OF THESE CONTAMINANTS IN THE SPACESUIT VENTILATION LOOP. IN PHASE I, WITH THE GUIDANCE OF MOLECULAR MODELING, WE WILL SYNTHESIZE SEVERAL SORBENTS AND EVALUATE THEIR POTENTIAL IN REVERSIBLE NH3 REMOVAL UNDER REPRESENTATIVE CONDITIONS. WE WILL ALSO EVALUATE THE EFFICACY OF THE AMBIENT TEMPERATURE OXIDATION CATALYST FOR FORMALDEHYDE REMOVAL AS WELL AS FOR OXIDATION OF OTHER VOCS. WE WILL DEMONSTRATE THE REGENERABLE SORBENT'S OPERATION FOR A MINIMUM OF 5,000 ADSORPTION/REGENERATION CYCLES AND ITS CATALYTIC ACTIVITY FOR A MINIMUM OF 400 HRS (EQUIVALENT OF 50 8HR EVAS). WE WILL EVALUATE THE IMPACT OF BED GEOMETRY AND POTENTIAL OF USING DIFFERENT INTEGRATION OPTIONS TO THE PLSS TO ENSURE THAT THE ADDITION OF THESE NEW MATERIALS WILL NOT IMPACT THE OPERATION OF THE SWING BED THAT REMOVES CARBON DIOXIDE. WE WILL CARRY OUT DETAILED DESIGN OF THE TCCS AND DETERMINE ITS WEIGHT/VOLUME TO ASSESS THE LOGISTICS SAVINGS AGAINST THE ONE-TIME USE NH3/CH2O REMOVAL SORBENTS.$125K
May 6, 2016National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CL10C541712IGF::OT::IGF POLYETHYLENE, AND ULTRAHIGH MOLECULAR WEIGHT POLYETHYLENE (UHMWPE) IN PARTICULAR, IS AN OUTSTANDING MATERIAL FOR RADIATION SHIELDING IN THE SENSE THAT ITS EXTRAORDINARILY HIGH HYDROGEN CONTENT BOTH MINIMIZES THE PRODUCTION OF SECONDARY IONS DURING EXPOSURE TO ENERGETIC RADIATION AND CAPTURES NEUTRONS. ITS LOW DENSITY AND HIGH WEAR RESISTANCE ALSO MAKE IT ATTRACTIVE FOR THE STRUCTURES OF MANNED SPACECRAFT AND EXTRATERRESTRIAL HABITATS. HOWEVER, ITS USE IN STRUCTURES IS LIMITED BY ITS FLAMMABILITY AND POOR MECHANICAL PROPERTIES UNDER LOAD COMPARED TO OTHER STRUCTURAL MATERIALS. WHILE CARBON FIBER/UHMWPE ARE AN OBVIOUS SOLUTION, TO DATE THEY HAVE NOT PROVED USEFUL BECAUSE LOAD IS NOT EASILY TRANSFERRED TO OR FROM UHMWPE, AND BECAUSE ITS MELT STATE IS TOO VISCOUS TO INFILTRATE FIBER PREFORMS. IN THIS PHASE II PROJECT, TDA WILL APPLY ITS RECENT ADVANCES IN COMPOSITE MANUFACTURING TO CREATE A UHMWPE-MATRIX COMPOSITE THAT HAS GOOD LOAD TRANSFER TO A CREEP-MITIGATING CONTINUOUS FIBER REINFORCEMENT. SUCH A COMPOSITE WILL NOT ONLY HAVE OUTSTANDING RADIATION SHIELDING PROPERTIES, BUT ALSO HAVE SUFFICIENT MECHANICAL PROPERTIES TO BE USEFUL AS A STRUCTURAL MATERIAL.$750K
May 5, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH11C0506541712PHASE II EXTENSION CPP$132K
May 3, 2016Department of DefenseW6QK ACC-APGW91CRB16C0023541712VECTOR PROTECTION - DETERMINATION OF ACTIVE INGREDIENT LEVELS FOR A NEW PYRETHROID UNIFORM TREATMENT FORMULATION$287K
Apr 26, 2016Department of DefenseW6QK ACC-APG DURHAMW911NF16C0073541712IGF::OT::IGF SBIR PHASE II$746K
Mar 31, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001415C0042541712ALUMINUM ALLOY CORROSION CONTROL AND PREVENTION$343K
Mar 14, 2016Department of DefenseW6QK ACC-RSAW31P4Q16C0060541712IGF::OT::IGF$100K
Feb 26, 2016Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833515C0278541712SBIR PHASE I TOPIC N151-025 IGF::OT::IGF$70K
Feb 18, 2016Department of DefenseW4PZ USA MED RSCH ACQUIS ACTW81XWH13C0157541712STTR PHASE I - A13A-019-0258$510K
Feb 12, 2016Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZLFA865016M6683541712IGF::OT::IGF SBIR I: VAPOR AND AEROSOL WEARABLE PASSIVE DOSIMETER$150K
Feb 4, 2016Department of DefenseOFFICE OF NAVAL RESEARCHN0001415C0042541712ALUMINUM ALLOY CORROSION CONTROL AND PREVENTION$25K
Dec 17, 2015Department of DefenseMISSILE DEFENSE AGENCY (MDA)HQ014716C7527541712IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT$100K
Dec 4, 2015National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTERNNX16CJ56C541712IGF::OT::IGF THE ORION MULTI-PURPOSE CREW VEHICLE (MPCV) NEEDS AN EMERGENCY BREATHING SYSTEM, IN THE EVENT THAT THE CABIN ATMOSPHERE BECOMES CONTAMINATED FROM A CHEMICAL SPILL, OR FROM A FIRE. THE EMERGENCY BREATHING NEEDS FOR ORION ARE SIMILAR TO, BUT NOT THE SAME AS, THE EMERGENCY BREATHING NEEDS ON ISS. ISS IS A LARGE VEHICLE, WITH A SLOW CLEANUP TIME - IT NEEDS UP TO 8 HOURS OF BREATHING PROTECTION. BUT BECAUSE ISS HAS A SERIES OF SAFE HAVENS AND ISOLATION HATCHES, THE ASTRONAUT CAN RETREAT FROM THE MOST AFFECTED AREA. THE ORION SPACECRAFT IS SMALL, AND IT HAS NO SAFE HAVENS OR ISOLATION HATCHES. SMALL SPILLS GENERATE HIGH CONCENTRATIONS OF CONTAMINANTS - BUT THE CONTAMINATED AIR CAN BE PURIFIED IN LESS THAN AN HOUR. THIS PROJECT INTENDS TO DESIGN AND EVALUATE AN EMERGENCY BREATHING SYSTEM THAT IS SPECIFICALLY DESIGNED TO MEET THE NEEDS OF ORION: IT WILL DEPLOY IN LESS THAN 15 SECONDS, IT WILL PROTECT THE CREW FROM HOT GAS INHALATION HAZARDS - EVEN IF THE CARBON MONOXIDE CONCENTRATION EXCEEDS 1%, IT WILL WEIGH LESS THAN 3 LBS, AND IT WILL OFFER LESS THAN 70 MMH2O BREATHING RESISTANCE AFTER 1 HOUR OF USE IN A POST-FIRE ENVIRONMENT.$185K
Oct 21, 2015Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIVN6833516C0044541712SBIR PI R&D. IGF::OT::IGF$80K

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