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Awards for “PHYSICAL SCIENCES INC.

25 awards on this page · sorted by amount · page 40

Federal prime contract awards for PHYSICAL SCIENCES INC.
Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
FA930008M3015PHYSICAL SCIENCES INC.Department of Defense$99.93K
2008-06-272014-10-16541712SBIR PHASE I
HQ014712C7869PHYSICAL SCIENCES INC.Department of Defense$99.92K
2012-01-182020-07-31541712PH I RESEARCH&DEVELOPMENT
NNX09CD30PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.92K
2009-01-222009-07-22541712SILICON WHISKER AND CARBON NANOFIBER COMPOSITE ANODE PHYSICAL SCIENCES INC. (PSI) PROPOSES TO DEVELOP A SILICON WHISKER AND CARBON NANOFIBER COMPOSITE ANODE FOR LITHIUM ION BATTERIES ON A PHASE I PROGRAM. THIS ANODE PROVIDES HIGH CAPACITY, HIGH POWER, AND IMPROVED CYCLE LIFE AT A COMPETITIVE COST. SILICON IS LOW COST AND HAS A THEORETICAL CAPACITY OF 4200 MAH/G BUT IT HAS A LIMITED CYCLE LIFE. THE NANOCOMPOSITE DESIGN PROVIDES A SYNERGISTIC IMPROVEMENT IN REVERSIBLE CAPACITY AND ELECTROCHEMICAL CYCLING AS A RESULT OF THE UNIQUE SILICON ARCHITECTURE AND STRUCTURAL REINFORCEMENT PROVIDED BY THE NANOFIBERS. IN THE PHASE I PROGRAM, PSI WILL DEMONSTRATE A TECHNOLOGY READINESS LEVEL OF 3 WITH AN ANODE CAPACITY OF GREATER THAN 1000 MAH/G FOR OVER 100 CYCLES (100% DEPTH-OF-DISCHARGE) USING 2 MAH CELLS. THESE PERFORMANCE GOALS WILL RESULT IN AN OVERALL BATTERY ENERGY DENSITY OF GREATER THAN 300 WH/KG. IN THE PHASE II PROGRAM, PSI WILL INCREASE CELL SIZE TO 2500 MAH AND OPTIMIZE CELL DESIGN TO FURTHER IMPROVE CYCLE LIFE.
FA930007M3104PHYSICAL SCIENCES INC.Department of Defense$99.92K
2007-05-212008-03-20541712NOVEL ENERGETIC BINDER FOR SOLID PROPELLANTS
HQ000610C7335PHYSICAL SCIENCES INC.Department of Defense$99.92K
2010-05-032010-11-02541712PH I RESEARCH & DEVELOPMENT
FA945311M0108PHYSICAL SCIENCES INC.Department of Defense$99.92K
2011-02-182012-02-20541712INTEGRATED OPTICAL WAVEGUIDES FOR SATELLITE OPTICAL COMMUNICATIONS RECEIVERS
HQ014713C7356PHYSICAL SCIENCES INC.Department of Defense$99.92K
2013-03-272013-09-28541712IGF::OT::IGF PH I RESEARCH&DEVELOPMENT TITLED: TAGGANT-FREE SECURE COMPONENT IDENTIFICATION.
FA955009C0028PHYSICAL SCIENCES INC.Department of Defense$99.92K
2008-11-012009-07-31541712(STTR PHASE I) ROBUST MAV DESIGN AND CONTROL USING BIOMIMETIC PRINCIPLES
HQ014713C7355PHYSICAL SCIENCES INC.Department of Defense$99.92K
2013-02-072013-08-10541712PH I RESEARCH&DEVELOPMENT TITLED: ENDO-ATMOSPHERIC AERO-THERMAL DEBRIS SURVIVAL AND GROUND PREDICTION MODEL IGF::OT::IGF
NNX09CD21PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.92K
2009-01-222009-07-22541712HIGH PERFORMING, LOW TEMPERATURE OPERATING, LONG LIFETIME, AEROSPACE LUBRICANTS PHYSICAL SCIENCES INC. (PSI) PROPOSES TO SYNTHESIZE, CHARACTERIZE, AND TEST NEW IONIC LIQUIDS AND FORMULATIONS AS LUBRICANTS FOR AEROSPACE APPLICATIONS. THE COMPOUNDS WILL OPERATE EFFECTIVELY AT LOW TEMPERATURES WITH APPROPRIATE VISCOSITIES, HIGH VISCOSITY INDICES, LARGE HEAT CAPACITIES, AND HIGH THERMAL DECOMPOSITION TEMPERATURES. THE INNOVATIVE, VERSATILE, LUBRICANTS WILL ALSO HAVE AN EXTREMELY WIDE LIQUIDUS RANGE, NEARLY ZERO VAPOR PRESSURE, LOW FRICTION COEFFICIENTS, SMALL WEAR EFFECTS, AND LOW OUTGASSING FOR LONG-TERM OPERATIONAL STABILITY IN AEROSPACE SYSTEMS. IN THE PHASE II PROGRAM, ADDITIONAL IONIC LIQUIDS WILL BE IDENTIFIED, SYNTHESIZED, CHARACTERIZED, FORMULATED WITH VARIOUS ADDITIVES, AND TESTED AS LIQUID LUBRICANTS AND BASE LUBRICANTS IN GREASES FOR USE AT LOW TEMPERATURE. THEIR TRIBOLOGICAL PERFORMANCE WILL BE EVALUATED IN AN AEROSPACE SYSTEM(S) FOR TRL 3.
N0001410M0180PHYSICAL SCIENCES INC.Department of Defense$99.92K
2010-05-102011-05-07541712RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
NNX11CI11PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.9K
2011-02-182012-02-18541712PHYSICAL SCIENCES INC. (PSI) TOGETHER WITH THE UNIVERSITY OF CONNECTICUT (UCONN) PROPOSES TO DEMONSTRATE THE IMPROVED FUEL CELL CATALYST SUPPORT DURABILITY OFFERED BY DIRECTLY INCORPORATING NITROGEN FUNCTIONALITY INTO GRAPHITIC CARBON SUPPORTS. IN PHASE I, PSI WILL UTILIZE THE FUNCTIONALIZED CARBON SUPPORT IN THE CONSTRUCTION OF SINGLE CELL FUEL CELLS IN ORDER TO DEMONSTRATE THE PERFORMANCE AND DURABILITY OF THE SUPPORT MATERIAL IN THE PEM FUEL CELL ENVIRONMENT. THE PERFORMANCE OF CELLS UPON ACCELERATED LIFE TESTING WILL BE CHARACTERIZED AND COMPARED WITH THAT OF CELLS ASSEMBLED USING COMMERCIALLY AVAILABLE SUPPORT MATERIALS TO QUANTIFY THE BENEFITS OFFERED BY THE FUNCTIONALIZED SUPPORT. IN PHASE II, PSI WILL WORK WITH UCONN TO OPTIMIZE AND SCALE-UP THE SUPPORT PRODUCTION PROCESSES. INCORPORATION OF ADDITIONAL FUNCTIONALITIES WILL ALSO BE INVESTIGATED. DEMONSTRATION CELLS WILL BE CONSTRUCTED AND DELIVERED FOR FUNCTIONAL AND ENVIRONMENTAL TESTING AT THE COMPLETION OF THE PHASE II CONTRACT.
FA955010C0065PHYSICAL SCIENCES INC.Department of Defense$99.9K
2010-04-012010-12-31541712(STTR PHASE I) PARALLEL FABRICATION OF MAGNETIC NANOCOMPUTING ARCHITECTURES BY ELECTROSPINNING
N6553809M0017PHYSICAL SCIENCES INC.Department of Defense$99.9K
2008-11-242009-12-30541712FIRST STATUS REPORT
N6553807M0166PHYSICAL SCIENCES INC.Department of Defense$99.9K
2007-06-212008-08-20541712FIRST STATUS REPORT
W9113M04P0069PHYSICAL SCIENCES INC.Department of Defense$99.9K
2004-05-052010-09-16541710200408!001577!2100!W9113M!USA SPACE AND STRATEGIC DEF CDR !W9113M04P0069 !A!N! !N! ! !20040505!20041105!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUSINESS CE!ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000099899!N!N!000000000000!AC23!RDTE/MISSILE AND SPACE SYSTEMS-ADV TECH DEV !A2 !MISSILE AND SPACE SYSTEMS !CAA !MDA SUPPORT !541710!E! !9! ! ! ! ! !99990909!C! ! !B! !A!N!J!2!077! ! !Z!N!Z! ! !N!B!N!N! ! !A! !A!A!00 !B!B!N! ! ! ! ! ! !0001! !
NNX11CE21PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.88K
2011-02-182011-09-29541712PHYSICAL SCIENCES INC. AND AMPAC IN-SPACE PROPULSION PROPOSE TO DEVELOP A UNIQUE CHEMICAL PROPULSION SYSTEM FOR THE NEXT GENERATION NASA SCIENCE SPACECRAFT AND MISSIONS THAT IS COMPACT, LIGHTWEIGHT, AND CAN OPERATE WITH HIGH RELIABILITY OVER EXTENDED PERIODS OF TIME AND UNDER WIDE RANGE OF THERMAL ENVIRONMENTS. THE SYSTEM USES A STORABLE, LOW TOXICITY, MONOPROPELLANT AS ITS WORKING FLUID. UNDER THIS SBIR PROGRAM WE PROPOSE TO INVESTIGATE APPLICATIONS OF THIS MONOPROPELLANT TO THE DESIGN OF IN-SPACE PROPULSION SYSTEMS APPROPRIATE FOR NASA PLANETARY SPACECRAFT AND MISSIONS. IN PHASE I, WE PROPOSE TO EXPERIMENTALLY CHARACTERIZE THE PROPELLANT IGNITION AND COMBUSTION PROCESSES IN DETAIL AND USE THE DATA TO DEVELOP DESIGN CONCEPTS FOR A LIQUID MONOPROPELLANT THRUSTER. IN PHASE II, WE PROPOSE TO DEVELOP AND DELIVER A SMALL SCALE PROOF-OF-CONCEPT ENGINEERING PROTOTYPE THRUSTER. UPON SUCCESSFUL TECHNOLOGY DEVELOPMENT UNDER THE SBIR PROGRAM, FULL-SCALE PROTOFLIGHT AND SPACE FLIGHT PROPULSION SYSTEMS APPLICABLE TO SPECIFIC MISSIONS WILL BE DEVELOPED IN PHASE III NASA PROGRAMS.
N0001409M0251PHYSICAL SCIENCES INC.Department of Defense$99.87K
2009-05-142010-11-30541712RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
N6553810M0100PHYSICAL SCIENCES INC.Department of Defense$99.87K
2010-04-152010-10-25541712FIRST STATUS REPORT
140D6318C0013PHYSICAL SCIENCES INC.Department of the Interior$99.85K
2017-11-292018-08-28541715SWITCHABLE LWIR FILTER USING PHASE-CHANGE MATERIALS
NNX11CF17PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.84K
2011-02-182011-09-29541712SPACE MISSIONS COULD BENEFIT FROM IMPROVED LUBRICANT TECHNOLOGY. PSI INTENDS TO DEVELOP NOVEL LIQUID LUBRICANT FORMULATIONS WHICH ARE APPLICABLE FOR FUTURE NASA MISSIONS. OUR CONCEPT IS BASED UPON USE OF NANOFLUID TECHNOLOGY WHEREBY STABLE, COLLOIDAL SUSPENSIONS OF ADDITIVES ARE PRESENT IN PERFLUOROPOLYALKYLETHER (PFPE) BASE FLUIDS. THE ADDITIVES WILL BECOME SHEARED WITHIN MINUTE SCRATCHES AND GROOVES WHILE SEPARATING SURFACE ASPERITIES. AT THE CONCLUSION OF PHASE I, WE WILL HAVE PREPARED ~ 10 NM DIAMETER ADDITIVES WITH ~ 115 M2/G AND ~ 80 M2/G GRAVIMETRIC SURFACE AREAS, RESPECTIVELY. THEIR SURFACE WILL HAVE BEEN CHEMICALLY MODIFIED AND SHOWN STABLE FROM -65OC TO +65OC. A 50% REDUCTION IN FRICTION AND WEAR AT STEEL SURFACES UPON DISPERSION OF THE ADDITIVE TO PFPE WILL HAVE BEEN DEMONSTRATED. PSI WILL HAVE SHOWN THAT THE VISCOSITY OF UNIFLOR 8960 PFPE IS MAINTAINED AT 60 CST 5% UPON FORMULATION WITH THE ADDITIVE. PSI WILL HAVE DEMONSTRATED THAT THE PARTICLES MAINTAIN AN AVERAGE PARTICLE SIZE OF ~ 10 NM WITHIN PFPE, AND WOULD HAVE SETTLING TIMES>5 YEARS. THE TRL AT THE BEGINNING OF THE PHASE I CONTRACT WILL BE AT 2, WHILE THE TRL AT THE COMPLETION OF THE PHASE I CONTRACT WILL BE AT 3-4.
NNX11CG55PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.81K
2011-02-182011-09-29541712PHYSICAL SCIENCES INC. PROPOSES TO DEVELOP A COMPACT, MULTIWAVELENGTH LIDAR WITH POLARIZATION ANALYSIS CAPABILITY THAT WILL BE ABLE TO IDENTIFY VOLCANIC ASH CLOUDS AT DISTANCE. THE SYSTEM WILL BE DEVELOPED SPECIFICALLY FOR AIRBORNE DEPLOYMENT, INCLUDING ON UNMANNED AERIAL SYSTEMS. A UAS-EQUIPPED WITH SUCH A LIDAR COULD PROVIDE VALUABLE SUPPLEMENTARY INFORMATION TO THAT AVAILABLE FROM EXISTING AND PLANNED SATELLITE ASSETS FOR DEFINING AND TRACKING VOLCANIC ASH PLUMES. THE SYSTEM FOOTPRINT WILL BE MINIMIZED BY TAKING ADVANTAGE OF ALL SOLID-STATE LASER TRANSMITTERS SUCH AS EMERGING METAL DOPED FIBER AMPLIFIERS. THE PHASE I PROGRAM WILL DETERMINE THE MOST APPROPRIATE WAVELENGTHS FOR USE VIA SYSTEM MODELING AND THEN WILL SELECT LASER TRANSMITTER HARDWARE. ADDITIONAL MODELING WILL DETERMINE THE TRANSMIT PULSE ENERGY AND RECEIVE APERTURE SIZE. THE SYSTEM WILL BE DESIGNED TO BE EYESAFE. A COMPLETE CONCEPTUAL DESIGN FOR AN AIRBORNE MULTIWAVELENGTH LIDAR WILL BE DEVELOPED. THE TECHNOLOGY READINESS LEVEL AT THE ENTRANCE TO THE PHASE I PROGRAM IS ESTIMATED TO BE 2 AND AT THE EXIT OF THE PROGRAM WILL BE 3. THE PHASE II PROGRAM WILL DESIGN, FABRICATE AND GROUND TEST A PROTOTYPE LIDAR SYSTEM. OPPORTUNITIES FOR A FLIGHT DEMONSTRATION WILL BE IDENTIFIED.
N6553810M0092PHYSICAL SCIENCES INC.Department of Defense$99.8K
2010-04-132011-05-31541712FIRST STATUS REPORT
NNX11CE31PPHYSICAL SCIENCES INC.National Aeronautics and Space Administration$99.77K
2011-02-182011-09-29541712PHYSICAL SCIENCES INC. PROPOSES TO DESIGN, DEVELOP, AND DEMONSTRATE, A NOVEL HIGH PERFORMANCE MONOPROPELLANT FOR APPLICATION IN FUTURE PLANETARY ASCENT VEHICLES. OUR NON-CARCINOGENIC, NON-CRYOGENIC, MONOPROPELLANTS WILL SIGNIFICANTLY AUGMENT SPECIFIC IMPULSE AND DENSITY SPECIFIC IMPULSE OVER CONVENTIONAL MONOPROPELLANT AND BI-PROPELLANT SYSTEMS. IN PHASE I, THE PROPOSED INVESTIGATION WILL FOCUS UPON CHARACTERIZING CRITICAL THERMAL AND CHEMICAL BEHAVIOR OF OUR MONOPROPELLANTS TO ENSURE REALISTIC SYSTEM LEVEL DESIGN AND MAXIMUM PERFORMANCE OF FUTURE PLANETARY ASCENT VEHICLES.
W9113M09C0103PHYSICAL SCIENCES INC.Department of Defense$99.5K
2009-03-272009-09-27541712MDA BASIC EFFORT - SBIR PAHSE I