Award search
Awards for “PHYSICAL SCIENCES INC.”
25 awards on this page · sorted by amount · page 15
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| FA930019C2003 | PHYSICAL SCIENCES INC. | Department of Defense | $749.96K | 2019-03-27 | 2021-06-25 | 541715 | MODULAR MICRO-REACTOR SYNTHESES OF HEH, HEHN AND HAN - SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II |
| FA864921P1493 | PHYSICAL SCIENCES INC. | Department of Defense | $749.96K | 2021-08-02 | 2023-03-03 | 541715 | SMALL BUSINESS INNOVATION RESEARCH PHASE II - DEVELOPMENT OF A COMPACT FABRY PEROT ETALON |
| W911SR14C0024 | PHYSICAL SCIENCES INC. | Department of Defense | $749.95K | 2014-04-16 | 2016-04-15 | 541712 | IGF::OT::IGF PHASE II STTR PSI |
| FA910121C0011 | PHYSICAL SCIENCES INC. | Department of Defense | $749.94K | 2021-03-19 | 2023-06-19 | 541715 | SBIR PHASE II A VERSATILE HYBRID MWIR SCENE PROJECTOR FOR TESTING OF ADVANCED FOCAL PLANE ARRAYS |
| FA864921P1640 | PHYSICAL SCIENCES INC. | Department of Defense | $749.93K | 2021-08-13 | 2023-02-13 | 541715 | ADDITIVELY MANUFACTURED SCRAMJET ASSEMBLIES |
| W911SR07C0068 | PHYSICAL SCIENCES INC. | Department of Defense | $749.93K | 2007-09-07 | 2009-09-08 | 541712 | RAPID CONCENTRATION OF PARTICLES |
| 80NSSC18C0107 | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $749.92K | 2018-04-11 | 2021-06-12 | 541715 | CURRENT MANNED AND UNMANNED SPACECRAFT REQUIRE SOPHISTICATED THERMAL CONTROL TECHNOLOGIES TO KEEP SYSTEMS AT TEMPERATURES WITHIN THEIR PROPER OPERATING RANGE. FUTURE MANNED AND UNMANNED MISSIONS TO THE MOON, MARS, AND OTHER DESTINATIONS WILL REQUIRE NEW TECHNOLOGIES TO MAINTAIN SPACECRAFT TEMPERATURE NEAR A SET-POINT WHILE UNDER VARIABLE HEAT LOADS AND THERMAL ENVIRONMENTS UNDER INCREASINGLY STRINGENT SIZE, WEIGHT AND POWER CONSTRAINTS. PASSIVE COMPONENTS, SUCH AS COATINGS WITH VARIABLE EMISSIVITY, CAN GREATLY EXTEND AND EXPAND NASA MISSION CAPABILITIES. PHYSICAL SCIENCES INC. WILL DEVELOP A PASSIVE THERMAL CONTROL SKIN (TCS) WITH A CONSTANT EMISSIVITY FROM 8 C TO 30 C AND AN INFRARED TURNDOWN RATIO OF GREATER THAN 8 BETWEEN 8 C AND -10 C. THE TCS WILL CONTROL BOTH THE INFRARED EMISSIVITY AS A FUNCTION OF THERMAL LOAD WHILE MAINTAINING A LOW SOLAR ABSORPTIVITY AT ALL RADIATOR TEMPERATURES. |
| N0002409C4131 | PHYSICAL SCIENCES INC. | Department of Defense | $749.91K | 2009-02-11 | 2012-01-12 | 541710 | N07-057 |
| FA865005C2610 | PHYSICAL SCIENCES INC. | Department of Defense | $749.91K | 2005-05-05 | 2009-09-04 | 541710 | 200508!002080!5700!FA8650!DET 1 AFRL/PK !FA865005C2610 !A!N! !Y! ! !20050505!20070817!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUS CTR DR !ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000375000!N!N!000000749909!AC16!RDTE/AIRCRAFT-MANAGEMENT SUPPORT !A1B!AIRCRAFT ENGINES AND SPARES !000 !* !541710!E! !3! ! ! ! ! !20200930!B! ! !A! !A!N!U!2!001!K! !Z!N!Z! ! !N!B!N!N! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| FA865119C0051 | PHYSICAL SCIENCES INC. | Department of Defense | $749.9K | 2019-02-13 | 2021-11-15 | 541715 | INTENSITY -DEPENDENT INFRARED BLOCKING FILTER FOR SOURCE EXCLUSION |
| FA955009C0075 | PHYSICAL SCIENCES INC. | Department of Defense | $749.9K | 2008-11-15 | 2010-11-14 | 541712 | STTR (PHASE II) - ATOMIC LAYER DEPOSITION OF ATOMIC OXYGEN RESISTANT, STATIC DISSIPATIVE COATINGS FOR SPACECRAFT |
| FA865008C6866 | PHYSICAL SCIENCES INC. | Department of Defense | $749.89K | 2008-04-18 | 2010-12-30 | 541720 | RAPID DEV |
| 80NSSC17C0017 | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $749.88K | 2017-09-25 | 2020-05-25 | 541712 | IGF::OT::IGFPHYSICAL SCIENCES INC. (PSI), IN COLLABORATION PURDUE UNIVERSITY, PROPOSES TO DEVELOP A NOVEL LAUNCH PROPULSION TECHNOLOGY FOR RAPID INSERTION OF NANO/MICRO SATELLITES (~ 5-100 KG SCALE) INTO LOW EARTH ORBIT, WITH THE POTENTIAL TO LOWER THE CURRENT STATE-OF-THE-ART LAUNCH STAGE COST BY 2X. THE TECHNOLOGY EMPLOYS A PROPULSION SCHEME COMPRISING A STORABLE LIQUID OXIDIZER AND A UNIQUE SOLID FUEL WITH EXCELLENT MECHANICAL AND THERMOCHEMICAL PROPERTIES. THE PROPOSED APPLICATION TO LAUNCH VEHICLE STAGES WILL RESULT IN LOW-COST, MASS-EFFICIENT LAUNCH SYSTEMS AND WILL REDUCE TECHNICAL DEVELOPMENT RISK FOR NASA. THE FUEL AND OXIDIZER ARE COMMERCIALLY AVAILABLE AT LOW COST AS AN INEXPENSIVE ENGINEERING MATERIAL AND AS AN INDUSTRIAL CHEMICAL. BOTH HAVE HIGH DENSITY, ARE GREEN, AND THE SYSTEM HAS A HIGH SPECIFIC IMPULSE (>275S; VACUUM). THE OXIDIZER STORAGE, HANDLING, TRANSPORTATION, AND LOADING OPERATIONS ARE SIMPLER AND SAFER COMPARED TO CRYOGENIC/TOXIC PROPELLANTS. THE FOREGOING ATTRIBUTES ENABLE THE LOWER COST OF THE PROPOSED HYBRID LAUNCH VEHICLE STAGE. THE PERFORMANCE OF CURRENT HYBRIDS IS LIMITED BY THEIR TYPICALLY LOW FUEL REGRESSION RATES. IN PHASE I, WE INVESTIGATED TECHNIQUES FOR SIGNIFICANTLY AUGMENTING THE REGRESSION RATE, DEMONSTRATING ~ 3.5X INCREASE IN 30 LBF THRUSTER FIRINGS. USING THIS DATA, WE PERFORMED DESIGN TRADES FOR A HYBRID STAGE AS THE SECOND/UPPER LAUNCH VEHICLE STAGE. THE ENHANCED REGRESSION RATE ALLOWED A MORE COMPACT, LIGHTER, HIGHER THRUST-TO-WEIGHT STAGE THAN WOULD BE POSSIBLE WITH CURRENT HYBRIDS. IN PHASE II, WE WILL PERFORM DETAILED EXPERIMENTS TO OPTIMIZE PROPULSIVE PERFORMANCE ON THE SAME PHASE I HYBRID THRUSTER, AND DEMONSTRATE A LARGE SCALE (~1000 LBF) MOTOR, REPRESENTATIVE OF UPPER STAGES OF A LAUNCH VEHICLE INCORPORATING THE OPTIMIZED DESIGN. PHASE II WILL END WITH A FLIGHT PROTOTYPE DESIGN AND A PLAN FOR A SUB-ORBITAL FLIGHT TEST, OR A COMPREHENSIVE GROUND TEST IN SIMULATED ENVIRONMENT. |
| FA945318C0220 | PHYSICAL SCIENCES INC. | Department of Defense | $749.88K | 2017-10-17 | 2020-01-18 | 541715 | IGF::OT::IGF SCALABLE MICROWAVE DRIVEN JET BASED TEST BED FOR SIMULATED HYPERSONIC REENTRY EFFECTS ON MATERIALS |
| NNX12CA41C | Q-PEAK, INCORPORATED | National Aeronautics and Space Administration | $749.85K | 2012-04-30 | 2015-01-29 | 541712 | IGF::OT::IGF OTHER FUNCTION - FOR LIGHTWEIGHT AND POWER-EFFICIENT INSTRUMENTS THAT ENABLE ELEMENTAL AND/OR MINERALOGY ANALYSIS, Q-PEAK PROPOSES TO DEVELOP A COMPACT, ROBUST, AND EFFICIENT INSTRUMENT CAPABLE OF PERFORMING IMAGING SPECTROSCOPY, LASER-RAMAN SPECTROSCOPY (LRS) AND LASER INDUCED BREAKDOWN SPECTROSCOPY (LIBS). THE MAIN ADVANTAGE IN USING THESE TECHNIQUES FOR PLANETARY SCIENCE IS THE ABILITY TO RAPIDLY COLLECT A WEALTH OF CHEMICAL INFORMATION, BY SIMPLY DIRECTING A LASER BEAM ON REMOTE TARGETS OF INTEREST. NO SAMPLE PREPARATION IS NECESSARY. AS AN IMPORTANT COMPONENT OF THE RAMAN/LIBS INSTRUMENT IN PHASE I, WE DEVELOPED, BUILT AND TESTED A 1.5 CUBIC-INCH, Q-SWITCHED, SOLID STATE LASER FITTED WITH COMMERCIAL, OFF-THE-SHELF OPTICAL COMPONENTS. THE LASER PRODUCED ~1 MJ,<2 NS-DURATION PULSES AT 523-NM WAVELENGTH AND WAS USED TO ANALYZE A NORITE SAMPLE BY MEANS OF RAMAN/LIBS TECHNIQUES. IN PHASE II WE PROPOSE TO FURTHER MINIATURIZE AND RUGGEDIZE THE PHASE I LASER TO A SIZE OF<1 CUBIC INCH. WE WILL SCALE UP THE ENERGY-PER-PULSE UP TO 2 MJ AND TEST THE LASER IN A WIDE RANGE OF ENVIRONMENTS SUCH AS VIBRATION, VACUUM AND TEMPERATURE. WE WILL DESIGN AND TEST THE OPTICS IN A CHAMP INSTRUMENT MODIFIED TO ACCOMMODATE THE COMPACT LASER. THE TRL OF THE LASER WILL BE 6 AT THE CONCLUSION OF THE EFFORT. |
| W31P4Q07C0177 | PHYSICAL SCIENCES INC. | Department of Defense | $749.8K | 2007-05-31 | 2009-08-31 | 331315 | PER KO REQUEST TO PROCESS THIS PAST DUE REQUIREMENT PHASE 2 ACTION FOR 'HIGH POWER 3D BATTERIES FOR AUTONOMOUS SENSOR NETWORK' |
| FA955010C0044 | PHYSICAL SCIENCES INC. | Department of Defense | $749.78K | 2010-02-15 | 2012-02-14 | 541712 | (STTR PHASE II) ROBUST MAV DESIGN AND CONTROL USING BIOMIMETIC PRINCIPLES |
| W9132T10C0038 | PHYSICAL SCIENCES INC. | Department of Defense | $749.72K | 2010-08-09 | 2013-03-31 | 541712 | U435CFM SELF-HEALING, REINFORCED, MULTIFUNCTIONAL COMPOSITE MATERIAL |
| 80NSSC22CA034 | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $749.71K | 2022-03-04 | 2025-03-02 | 541715 | E014042 SBIR-STTR PHASE II INTELLIGENT SENSOR SYSTEM FOR ROCKET PROPULSION TESTING |
| W911SR13C0005 | PHYSICAL SCIENCES INC. | Department of Defense | $749.63K | 2013-02-14 | 2015-02-13 | 541711 | THIS IS A STTR PHASE II TITLED "REAL-TIME NON-CONTRACT DETECTION OF SURFACE CONTAMINATION." THIS CONTRACT IS TO DEVELOP THE CAPABILITY TO PREDICT WHAT THE INFRARED SPECTRA OF LIQUID CONTAMINATION ON SURFACES WILL BE AND TO USE IT TO DETECT THE CONTAMINATION. |
| 80NSSC19C0013 | PHYSICAL SCIENCES INC. | National Aeronautics and Space Administration | $749.6K | 2018-12-06 | 2021-06-04 | 541715 | PHYSICAL SCIENCES INC. AND PURDUE UNIVERSITY PROPOSE TO DEVELOP A NOVEL APPROACH TO SCAVENGING HEAT FROM HIGH INTENSITY THERMAL ENVIRONMENTS ENCOUNTERED DURING SPACE MISSIONS AND CONVERTING THIS THERMAL POWER TO ELECTRICAL POWER AT HIGH EFFICIENCY. EXAMPLES INCLUDE EXTREMELY HOT HEAT SHIELDS DURING VEHICLE ENTRY INTO PLANETARY ATMOSPHERES (MARS/VENUS PROBES) AND DURING HIGH SPEED ASCENT THROUGH PLANETARY ATMOSPHERES (SAMPLE RETURN FROM MARS/VENUS), HOT CLADDINGS OF RADIOISOTOPE THERMOELECTRIC GENERATORS USED FOR POWERING OUTER PLANETARY SPACECRAFT AND MULTI-DECADE PLANETARY BASES (MARS/VENUS/LUNAR), AS WELL AS COMBUSTORS/NOZZLES OF SPACE AND LAUNCH PROPULSION SYSTEMS, SPECIFICALLY, NUCLEAR PROPULSION SYSTEMS OF RENEWED INTEREST. THE TECHNOLOGY IS ALSO APPLICABLE COMMERCIALLY TO HIGH TEMPERATURE SOURCES ENCOUNTERED IN TERRESTRIAL SYSTEMS, SUCH AS PORTABLE ELECTRICAL POWER CONVERTERS FROM MACHINERY (ENGINES, STOVES) USED BY SOLDIERS AND CIVILIANS IN OUTDOOR ENVIRONMENTS, IN THIS STTR WE WILL DEVELOP AN INTEGRATED METAL HYDRIDE (MH) SYSTEM AND SPECTRALLY-TUNED THERMOPHOTOVOLTAIC POWER CONVERTER (PC) SYSTEM THAT CAN EXTRACT HEAT DURING PERIODS OF HIGH THERMAL INTENSITY AND CONVERT IT TO ELECTRICITY AT GREATER THAN 25 PERCENT EFFICIENCY. THE MH SYSTEM PROVIDES THE HIGH TEMPERATURE RESERVOIR NEEDED FOR PC OPERATION. |
| FA865013C1618 | PHYSICAL SCIENCES INC. | Department of Defense | $749.57K | 2013-05-02 | 2015-12-30 | 541712 | IGF::OT::IGF SBIR II - QUANTUM DOT BASED OPTICAL TAGGANTS FOR COMBAT |
| N0002411C4176 | PHYSICAL SCIENCES INC. | Department of Defense | $749.45K | 2011-08-26 | 2014-09-30 | 541712 | N093-201 NEW PH II AWD PEO SUB |
| FA865006C6647 | PHYSICAL SCIENCES INC. | Department of Defense | $749.29K | 2006-04-28 | 2008-07-27 | 541710 | 200607!005721!5700!FA8650!DET 1 AFRL/PK !FA865006C6647 !A!N! !Y! ! !20060428!20080310!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUS CTR DR !ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000250000!N!N!000000749924!AZ16!RDTE/OTHER RESEARCH & DEVELOPMENT-MGMT SUPPORT !C9E!ALL OTHER SUPPLIES AND EQUIPMENT !000 !NOT DISCERNABLE !541710!E! !3! ! ! ! ! !99990909!B! ! !N!Z!A!N!U!2!002!K! !Z!N!Z! ! !N!B!N!N! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! |
| FA865004C2484 | PHYSICAL SCIENCES INC. | Department of Defense | $749.24K | 2004-07-08 | 2011-08-02 | 541710 | 200410!000199!5700!GR06 !AFRL/PRKA AEROSPACE POWER FUELS !FA865004C2484 !A!N! !N! ! !20040708!20061130!073800062!073800062!073800062!N!PHYSICAL SCIENCES INC !20 NEW ENGLAND BUSINESS CE!ANDOVER !MA!01810!01430!009!25!ANDOVER !ESSEX !MASS !+000000375000!N!N!000000749995!AC12!RDTE/AIRCRAFT-APPLIED RESEARCH !A1C!OTHER AIRCRAFT EQUIPMENT !000 !* !541710!E! !3! ! ! ! ! !99990909!B! ! !A! !A!N!U!2!002!K! !Z!N!Z! ! !N!B!N!N! ! !Z! !B!A!00 !C!B!N! ! ! ! ! ! !0001! ! |