Award search
Awards for “PHYSICAL SCIENCES INC.”
25 awards on this page · sorted by amount · page 17
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| W911QX06C0138 | PHYSICAL SCIENCES INC. | Department of Defense | $730K | 2006-09-27 | 2010-06-30 | 541710 | SBIR PHASE II, TOPIC #:A05-048 |
| W912HZ09C0110 | PHYSICAL SCIENCES INC. | Department of Defense | $729.97K | 2009-09-11 | 2011-12-31 | 541712 | SBIR PROPOSAL NO. A2-3877; PHASE II; ENHANCED EVENT DETECTION WITH SEISMIC LISTENING SENSORS |
| W911SR11C0005 | PHYSICAL SCIENCES INC. | Department of Defense | $729.96K | 2010-12-30 | 2013-01-31 | 541711 | YEAR ONE SBIR PHASE II SERVICES - AWARD |
| W911SR12C0041 | PHYSICAL SCIENCES INC. | Department of Defense | $729.93K | 2012-03-08 | 2014-02-25 | 541711 | (TDLAS) PHASE II |
| W911SR11C0011 | PHYSICAL SCIENCES INC. | Department of Defense | $729.92K | 2011-02-16 | 2013-08-14 | 541711 | PHASE II SBIR |
| W31P4Q10C0110 | PHYSICAL SCIENCES INC. | Department of Defense | $729.91K | 2010-06-30 | 2012-12-31 | 541712 | ARMY SBIR PHASE II |
| W56HZV06C0580 | PHYSICAL SCIENCES INC. | Department of Defense | $729.84K | 2006-09-14 | 2010-04-30 | 541710 | 200612!009186!2100!W56HZV!TACOM - WARREN !W56HZV06C0580 !A!N! !Y! ! !20060914!20080914!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUS CTR DR !ANDOVER !MA!01810!81035!017!25!WOBURN !MIDDLESEX !MASS !+000000326111!N!N!000000000000!AC43!RDTE/TANK - AUTOMOTIVE-ADV TECH DEV !A4A!COMBAT VEHICLES !000 !NOT DISCERNABLE !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!N!U!2!053!K! !Z!Y!Z! ! !N!B!N!N! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| W15QKN06C0106 | PHYSICAL SCIENCES INC. | Department of Defense | $729.8K | 2006-01-31 | 2008-09-30 | 541330 | 200605!600297!2100!W15QKN!TACOM - PICATINNY !W15QKN06C0106 !A!N! !N! ! !20060131!20070129!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUS CTR DR !ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000380784!N!N!000000380784!AD91!RDTE/OTHER DEFENSE-BASIC RESEARCH !S1 !SERVICES !000 !NOT DISCERNABLE !541330!E! !3! ! ! ! ! !99990909!B! ! !N!Z!A!N!U!2!002!K! !Z!N!Z! ! !N!B!N!N! ! !A! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| W911SR06C0011 | PHYSICAL SCIENCES INC. | Department of Defense | $729.67K | 2006-01-25 | 2009-05-29 | 541710 | 200605!600260!2100!W911SR!USA MATERIEL COMMAND ACQUISITION!W911SR06C0011 !A!N! !N! ! !20060125!20080131!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUS CTR DR !ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000482577!N!N!000000729672!AD24!RDTE/SERVICES-DEMO/VALID !S1 !SERVICES !000 !* !541710!E! !3! ! ! ! ! !99990909!B! ! !A! !A!U!U!2!002!K! !Z!N!Z! ! !N!B!N!N! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| DAAD1303C0027 | PHYSICAL SCIENCES INC. | Department of Defense | $728.98K | 2003-04-24 | 2010-09-15 | 541710 | 200308!000552!2100!AD13 !USA MATERIEL COMMAND ACQUISITION!DAAD1303C0027 !A!N! !N! !20030424!20050422!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUSINESS CE!ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000364963!N!N!000000729686!AD92!RDTE/OTHER DEFENSE-APPLIED RESEARCH !S1 !SERVICES !1000!NOT DISCERNABLE OR CLASSIFIED !541710!E! !3! ! ! ! ! !99990909!B! ! !A! !A!U!U!2!001!K! !Z!N!Z! ! !N!B!U!N! ! !C! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| 0001 | PHYSICAL SCIENCES INC. | Department of Defense | $720K | 2009-09-30 | 2013-07-25 | 541712 | LEADR |
| NNX12CA24C | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $704.02K | 2012-04-30 | 2015-04-30 | 541712 | IGF::OT::IGF OTHER FUNCTION - PHYSICAL SCIENCES INC. (PSI) AND ORBITEC INC. 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 NEW STORABLE, LOW TOXICITY, LIQUID MONOPROPELLANT AS ITS WORKING FLUID. IN PHASE I, WE HAVE DEMONSTRATED EXPERIMENTALLY THE CRITICAL IGNITION AND COMBUSTION PROCESSES FOR THE PROPELLANT AND USED THE DATA TO DEVELOP THRUSTER DESIGN CONCEPTS. PHASE I WORK ACHIEVED TRL 3. IN PHASE II, WE PROPOSE TO DEVELOP AND DEMONSTRATE IN THE LABORATORY A PROOF-OF-CONCEPT PROTOTYPE THRUSTER. PHASE II WILL ACHIEVE TRL 4+. WE ENVISION FOLLOW-ON PHASE II ENHANCEMENT (PHASE II E) AND PHASE III PROGRAMS TO ADVANCE THE TRL TO 5 AND 6, RESPECTIVELY. PHASE III WILL BE THE DEVELOPMENT OF A FULL-SCALE PROTOFLIGHT PROPULSION SYSTEM APPLICABLE TO A CLASS OF NASA MISSIONS. ON BOTH PHASE II E AND PHASE III PROGRAMS, WE WILL COLLABORATE WITH SPECIFIC NASA PROGRAMS AND THE INDUSTRY TO ADDRESS THE COST SHARE COMPONENT. FOLLOWING A SUCCESSFUL PHASE III A SPACE FLIGHT DEMONSTRATION ON A NASA MISSION WILL ADVANCE THE TRL TO 7. |
| DEAC2295PC95101 | PHYSICAL SCIENCES INC. | Department of Energy | $702.09K | 1999-12-15 | 2001-06-30 | — | — |
| W911NF06C0137 | PHYSICAL SCIENCES INC. | Department of Defense | $700.09K | 2006-08-11 | 2009-06-10 | 541710 | NONWOVEN NANOFIBER MEMBRANES FOR PROTECTIVE GARMENTS |
| N0002425CS067 | PHYSICAL SCIENCES INC. | Department of Defense | $697.17K | 2025-07-29 | 2026-07-29 | 541713 | BASE AWARD, SBIR PHASE II TOPIC #N212-126 |
| F1962800C0077 | PHYSICAL SCIENCES INC. | Department of Defense | $686.31K | 2000-09-15 | 2010-10-05 | 541710 | 200012!5700!000256!GV03 !ESC/PKR R&D CONTRACTING !F1962800C0077 !A!*!* !20000915!20051231!073800062!073800062!073800062!N!8K901!PHYSICAL SCIENCES INC. !20 NEW ENGLAND BUSINESS CE!ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !0001!+000000041199!N!N!000000000000!AD91!RDTE/OTHER DEFENSE-BASIC RESEARCH !A7 !ELECTRONICS AND COMMUNICATION !3000!NOT DISCERNABLE OR CLASSIFIED !8731!3!*!*!*!B!A!*!A !N!U!2!002!E!* !Z!Y!Z!* !* !N!B!N!A!*!A!A!A!A!* !*!N!A!B!N!*!*!*!*!*! |
| N0001407C0177 | PHYSICAL SCIENCES INC. | Department of Defense | $649.88K | 2007-01-24 | 2010-07-21 | 541710 | RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES |
| FA955008C0026 | PHYSICAL SCIENCES INC. | Department of Defense | $646.82K | 2007-11-01 | 2009-10-31 | 541720 | STTR PHASE II |
| HSHQDC11C00117 | PHYSICAL SCIENCES INC. | Department of Homeland Security | $625.51K | 2011-09-07 | 2013-02-28 | 541712 | AWARD UNDER BAA BAA11-101 - DETECTION AND IDENTIFICATION OF RADIOLOGICAL THREATS IN LOW SCR CARGO SCREENING ENVIRONMENTS. |
| 70RWMD20F00000029 | PHYSICAL SCIENCES INC. | Department of Homeland Security | $619.22K | 2020-07-09 | 2022-03-15 | 541715 | PHYSICAL SCIENCES, INC. (PSI) TO PROVIDE THE DEPARTMENT OF HOMELAND SECURITY RESEARCH AND DEVELOPMENT SUPPORT SERVICES ISSUED UNDER DHS INDEFINITE DELIVERY INDEFINITE QUANTITY CONTRACT 70RDND19D00000001. |
| NNX10CA51C | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $600K | 2009-12-28 | 2011-12-27 | 541712 | PHYSICAL SCIENCES INC. (PSI) HAS SUCCESSFULLY DEVELOPED A SILICON WHISKER AND CARBON NANOFIBER COMPOSITE ANODE FOR LITHIUM ION BATTERIES ON A PHASE I PROGRAM. PSI HAS DEMONSTRATED A TECHNOLOGY READINESS LEVEL OF 3 WITH AN ANODE COMPOSITE CAPACITY OF GREATER THAN 1100 MAH/G FOR OVER 200 CYCLES (100% DEPTH-OF-DISCHARGE) AT 1C USING 2 MAH CELLS. 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 II PROGRAM, PSI WILL INCREASE CELL SIZE TO 2.5 MAH AND OPTIMIZE CELL DESIGN TO FURTHER IMPROVE CYCLE LIFE. PSI WILL DELIVER TO NASA 2.5 AH LITHIUM ION CELLS WITH AN ENERGY DENSITY GREATER THAN 220 WH/KG THAT IS REQUIRED BY NASA'S FUTURE ROBOTIC AND HUMAN EXPLORATION MISSIONS. IN COLLABORATION WITH A BATTERY MANUFACTURER, PSI WILL ALSO DEMONSTRATE THAT THIS ANODE TECHNOLOGY IS SCALEABLE TO REACH INDUSTRIAL PRODUCTION LEVEL. |
| NNX11CB77C | Q-PEAK, INCORPORATED | National Aeronautics and Space Administration | $600K | 2011-06-03 | 2013-09-02 | 541712 | THE PRIMARY OBJECTIVE OF THE PROPOSED PHASE II EFFORT IS TO DEVELOP AND DELIVER A RUGGEDIZED, SINGLE-FREQUENCY, MJ-LEVEL, 2050-NM MASTER OSCILLATOR POWER AMPLIFIER SYSTEM SUITABLE FOR COHERENT LIDAR APPLICATIONS. THE LASER SYSTEM IS BASED ON A LOW-AVERAGE POWER, PULSED, SINGLE-FREQUENCY, 2-UM HO-LASER SOURCE. PULSED OPERATION OF THE HO-OSCILLATOR IS ACHIEVED VIA PASSIVE Q-SWITCHING USING ROBUST CR2+-DOPED SATURABLE ABSORBERS. DEVELOPMENT OF SUCH PULSED SEED SOURCES ENABLES THE DESIGN OF COMPACT, RUGGED, RELIABLE AND EFFICIENT LIDAR TRANSMITTERS BASED ON ALL-AMPLIFIER ARCHITECTURE. DIRECT DIODE-PUMPING USING THE LATEST 1.9-UM DIODE LASER TECHNOLOGY PROVIDES IMPROVED OSCILLATOR RELIABILITY AND COMPACTNESS. EFFICIENT, TM:FIBER LASER PUMPED, BULK HO:YLF SINGLE-STAGE AMPLIFIER PROVIDES ENERGY SCALING TO MJ LEVEL. THE CHOICE OF A 2-UM HO-LASER MATERIAL (AS OPPOSED TO 1.5-UM ER-LASERS) ENABLES EFFICIENT POWER/ENERGY SCALING OF THE PULSED SEED OSCILLATOR OUTPUT IN HIGH-GAIN HO-AMPLIFIERS. THIS APPROACH DECREASES THE NUMBER OF AMPLIFYING STAGES, SIMPLIFIES THE OVERALL DESIGN AND PACKAGING, AND IMPROVES THE ELECTRICAL EFFICIENCY OF THE COMPLETE LASER SYSTEM AS COMPARED TO THE CURRENT TECHNOLOGY. |
| NNX10CB61C | MAXION TECHNOLOGIES, INC. | National Aeronautics and Space Administration | $599.99K | 2010-09-02 | 2015-10-01 | 541712 | TUNABLE, NARROW LINE WIDTH MID-INFRARED LASER SOURCE THE PURPOSE OF THIS PROJECT IS TO ADVANCE THE TECHNOLOGY OF INTERBAND CASCADE (IC) LASERS AND THEIR FACET COATINGS AND TO DESIGN, BUILD, AND DELIVER TO NASA A TUNABLE, NARROW LINEWIDTH MID-INFRARED LASER SOURCE OPERATING IN THE 3.2 V 3.6 MICRON WAVELENGTH BAND. INITIAL WORK WILL DEVELOP IMPROVED IC LASER ACTIVE REGIONS AS WELL AS ULTRA-LOW-REFLECTIVITY ANTI-REFLECTION FACET COATINGS. WE WILL ALSO DEVELOP AN EFFECTIVE EPI-SIDE-DOWN DIE ATTACH PROCESS FOR IC LASERS USING A AU/SN SOLDER. THE OBJECTIVE OF THIS INITIAL WORK IS TO ACHIEVE LASER CHIPS EMITTING IN THE APPROPRIATE WAVELENGTH REGION AND OPERATING IN CONTINUOUS WAVE MODE AT HEAT SINK TEMPERATURES>25C AND WITH SEVERAL 10S OF MW OF OUTPUT POWER. THE TEAM WILL THEN USE OUR EXTENSIVE EXPERIENCE WITH EXTERNAL CAVITY LASER SOURCES TO DESIGN, BUILD, AND DELIVER A VERSATILE, TUNABLE MID-INFRARED SOURCE TO NASA USING THE DEVELOPED IC LASER GAIN CHIP. THE DELIVERED TUNABLE LASER SOURCE WILL BE AT A TRL LEVEL OF 5 AND WILL ENABLE SENSITIVE EARTH SCIENCE TRACE GAS MEASUREMENTS AND ENHANCE NASA'S EXISTING MEASUREMENT CAPABILITY BY SIGNIFICANTLY IMPROVING THE SENSITIVITY AND PERFORMANCE OF TRACE GAS SENSING BY VIRTUE OF A CONSIDERABLY IMPROVED SOURCE TECHNOLOGY. |
| NNX10CA46C | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $599.99K | 2009-12-28 | 2012-03-11 | 541712 | PHYSICAL SCIENCES INC. (PSI) PROPOSES TO SYNTHESIZE, CHARACTERIZE, AND TEST NEW IONIC LIQUIDS AND FORMULATIONS AS LUBRICANTS FOR AEROSPACE APPLICATIONS. THE COMPOUNDS WILL HAVE LOW VAPOR PRESSURES/OUTGASSING AND APPROPRIATE THERMAL STABILITY. UPON ADDITION OF THE INNOVATIVE IONIC LIQUIDS TO THE BASE LUBRICANTS, A 20% DECREASE IN VISCOSITY, FRICTION COEFFICIENT, AND WEAR WILL RESULT. MINIMAL CORROSIVE EFFECTS OF THE FORMULATIONS AT WILL BE OBSERVED. THE FORMULATIONS WILL BE SHOWN MORE EFFECTIVE AS LIQUID LUBRICANTS FOR USE AT LOW TEMPERATURES (-70OC) WITH LONG-TERM OPERATIONAL STABILITY IN AEROSPACE SYSTEMS. SEVERAL NEW IONIC LIQUIDS WILL BE SCALED AND A NOVEL FORMULATION WILL BE EVALUATED IN A NASA TEST BED. THE TECHNOLOGY WILL BE AT A TRL RANGE FROM 3-4 UPON COMPLETION OF PHASE II. |
| NNX10RA22C | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $599.99K | 2009-11-10 | 2011-05-09 | 541712 | PHYSICAL SCIENCES INC. (PSI) HAS DEVELOPED A CERAMIC COMPOSITE MATERIAL SYSTEM THAT IS MORE EFFECTIVE FOR SHIELDING BOTH GCR AND SPE THAN ALUMINUM. THE COMPOSITE TECHNOLOGY ENABLES A MODULAR, MULTIFUNCTIONAL BUILDING SYSTEM FOR LUNAR HABITATS THAT CAN KEEP EQUIVALENT DOSES RECEIVED BY ASTRONAUTS BELOW THE 150 MSV EXPOSURE LIMIT DURING A 90 DAY LUNAR MISSION. DURING PHASE I, WE ACHIEVED TRL 3 BY DEMONSTRATING THAT OUR CERAMIC COMPOSITE MATERIAL IS SUPERIOR TO ALUMINUM IN RADIATION SHIELDING APPLICATIONS USING HZETRN CODE CALCULATIONS AND RADIATION EXPOSURE EXPERIMENTS ON MATERIAL TEST SAMPLES. THE PHASE II SBIR EFFORT WILL ADVANCE OUR CERAMIC COMPOSITE TO TRL 5 BY .. 1) PERFORMING DETAILED SHIELDING CALCULATIONS USING OLTARIS FOR A PROPOSED SHELTER WALL DESIGN 2) DEMONSTRATING FABRICATION METHODS THAT PRODUCE MATERIAL WITH CONSISTENT MECHANICAL, ELECTRICAL AND THERMAL PROPERTIES 3) USING RADIATION EXPOSURE EXPERIMENTS TO VERIFY SHIELDING PERFORMANCE WE WILL DESIGN AND ANALYZE A LUNAR HABITAT WALL SYSTEM USING OUR CERAMIC COMPOSITE MATERIAL AS THE PRIMARY STRUCTURAL MEMBER. WE WILL FABRICATE AND STRENGTH TEST OUR CERAMIC COMPOSITE MATERIALS TO DEMONSTRATE THAT THE CERAMIC COMPOSITE SYSTEM IS A VIABLE STRUCTURAL MATERIAL FOR LUNAR HABITATS. WE WILL DEMONSTRATE THAT THE CERAMIC COMPOSITE SYSTEM WILL PROVIDE AT LEAST 20% GREATER RADIATION SHIELDING EFFECTIVENESS AGAINST GCR AND SPE THAN AN ALUMINUM STRUCTURE OF COMPARABLE MASS. |