![]() | POWDERMET, INC. |
24112 ROCKWELL DR EUCLID OH 44117-1252 UNITED STATES Telephone: 2164040053 |
POWDERMET, INC. is an Active Manufacturer with the Cage Code 1CZU5 and is tracked by Dun & Bradstreet under DUNS Number 175863463.
SIC Code 1: | 3399 |
Status: | A |
Type: | A |
Size: | A |
Primary Business: | J |
Type of Business: | N |
Woman Owned: | N |
CAO: | S3605A |
ADP CNT CT: | HQ0337 |
T: TRAINING GRANT
NASA REQUIRES HIGH ENERGY DENSITY, HIGH VOLTAGE, HIGH POWER AND HIGH EFFICIENCY CAPACITOR THAT CAN BE INTEGRATED INTO THE SYSTEM TO DECREASE THE MASS AND SPACE AT THE SYSTEM ARCHITECTURE LEVEL AND INCREASE THE EFFICIENCY. THE CURRENT STATEOFTHEART OF THE CAPACITOR HAS LOW ENERGY, LOW POWER DENSITY AND LOW ENERGY STORAGE EFFICIENCY, MAKING THEM BULKY AND COSTLY FOR THE APPLIED SYSTEM. FOR THE NASA APPLICATION, IN ORDER TO MAINTAIN THE ENERGY OR POWER SYSTEM WORK PROPERTY, ONBOARD COOLING SYSTEMS HAS BEEN INSTALLED, WHICH IN TURN INCREASE THE MASS AND SPACE. THEREFORE, IT IS IMPORTANT TO DEVELOP IMPROVED CAPACITORS IN ENERGY DENSITY, SPEED, EFFICIENCY TO MINIMIZE THE SIZE AND MASS OF FUTURE POWR SYSTEM. IN THIS PROPOSAL, POWDERMET PROPOSED TO DEVELOP ANOTHER TYPE ADVANCED NANOCOMPOSITE CAPACITOR WITH ULTRAHIGH ENERGY DENSITY, HIGH VOLTAGE, HIGH POWER AND HIGH ENERGY STORAGE EFFICIENCY. THIS NOVEL CAPACITOR WILL FEATURE ULTRAHIGH ENERGY DENSITY (>40 J/CC), HIGH OPERATING VOLTAGE (>KILOVOLT), HIGH POWDER DENSITY (>MW/CC), ESPECIALLY HIGH ENERGY STORAGE EFFICIENCY (>95%
AR21: R&D- SPACE: SCIENCE/APPLICATIONS (BASIC RESEARCH)
B: PURCHASE ORDER
IGF::OT::IGF NASA REQUIRES HIGH ENERGY DENSITY, HIGH VOLTAGE, HIGH POWER AND HIGH EFFICIENCY CAPACITOR THAT CAN BE INTEGRATED INTO THE SYSTEM TO DECREASE THE MASS AND SPACE AT THE SYSTEM ARCHITECTURE LEVEL AND INCREASE THE EFFICIENCY. THE CURRENT STATE-OF-THE-ART OF THE CAPACITOR HAS LOW ENERGY, LOW POWER DENSITY AND LOW ENERGY STORAGE EFFICIENCY, MAKING THEM BULKY AND COSTLY FOR THE APPLIED SYSTEM. FOR THE NASA APPLICATION, IN ORDER TO MAINTAIN THE ENERGY OR POWER SYSTEM WORK PROPERTY, ONBOARD COOLING SYSTEMS HAS BEEN INSTALLED, WHICH IN TURN INCREASE THE MASS AND SPACE. THEREFORE, IT IS IMPORTANT TO DEVELOP IMPROVED CAPACITORS IN ENERGY DENSITY, SPEED, EFFICIENCY TO MINIMIZE THE SIZE AND MASS OF FUTURE POWER SYSTEM. IN THIS PROPOSAL, POWDERMET PROPOSED TO DEVELOP ANOTHER TYPE ADVANCED NANOCOMPOSITE CAPACITOR WITH ULTRA-HIGH ENERGY DENSITY, HIGH VOLTAGE, HIGH POWER AND HIGH ENERGY STORAGE EFFICIENCY. THIS NOVEL CAPACITOR WILL FEATURE ULTRA-HIGH ENERGY DENSITY (>40 J/CC), HIGH OPERATING VOLTAGE (>KILOVOLT), HIGH POWDER DENSITY (>MW/CC), ESPECIALLY HIGH ENERGY STORAGE EFFICIENCY (>95%).
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
B: PURCHASE ORDER
IGF::OT::IGF DURING SPACE-FLIGHT SYSTEM DESIGN, CHOICE IN ELECTRONIC COMPONENTS/DEVICES IS AN IMPORTANT CHOICE WHEN CONSIDERING MAXIMUM FAILURE TOLERANCE FROM SPACE RADIATION EFFECTS. A TECHNOLOGY THAT CAN PROVIDE ENHANCED RELIABILITY OF FLIGHT ELECTRONICS BY SIGNIFICANTLY REDUCING EXPOSED RADIATION DAMAGE WITH MINIMUM SHIELD MASS OFFERS IMPROVED CHANCES FOR MISSION SUCCESS, AND THUS REDUCING SYSTEM ERRORS, SAVING PROGRAM COST AND RESOURCES. POWDERMET PROPOSES THE DEVELOPMENT OF A GRADIENT-Z POWDER ADDITIVE FOR PLASTICS THAT CAN TRANSFORM THEM INTO EFFECTIVE RADIATION SHIELDS. THE ELECTIVE EASE OF RADIATION HARDENING OFF-THE-SHELF ELECTRONICS WITH AN EASILY APPLIED SHIELDING ENCAPSULATE REDUCES COST AND TIME TO LAUNCH. THE TECHNICAL APPROACH WILL BE IN THE COMPUTATIONAL VALIDATION AND EXPERIMENTAL VERIFICATION OF A GRADIENT-Z MICROPOWDER COMPOSITE ADDITIVE FOR GRANTING RADIATION SHIELDING TO PLASTICS. THESE WILL BE COMPARED TO CONVENTIONAL GRADIENT-Z METAL LAY-UP DESIGNS. ADDITIONAL, THE PROGRAM WILL DEMONSTRATE THE ADDITIVE MANUFACTURING CAPACITY OF GRADIENT-Z MICROPOWDER COMPOSITES.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
D: DEFINITIVE CONTRACT
IGF::OT::IGF THE TECHNICAL APPROACH PROPOSED IN THE PHASE II PROGRAM BUILDS ON THE ENCOURAGING RESULTS OF THE PHASE I PROGRAM, IN THE EXCELLENT ENERGY STORAGE PERFORMANCE OVER A BROAD TEMPERATURE RANGE. IN THIS PHASE II PROGRAM, THE PROPOSAL NANOCOMPOSITE FILMS WILL BE FEATURE AS HIGH ENERGY DENSITY (>12 J/CC), DIELECTRIC BREAKDOWN STRENGTH (>600 MV/M), HIGH WIDE OPERATING VOLTAGE (HUNDRED VOLT TO KILOVOLT), HIGH POWER DENSITY (>4 MW/CC) AS WELL AS HIGH ENERGY STORAGE EFFICIENCY (>96%). THE CAPACITOR ENERGY STORAGE MODULE FABRICATED FROM THE DEVELOPED FILMS WILL BE FEATURE AS HIGH ENERGY DENSITY (>5 J/CC), HIGH WIDE OPERATING VOLTAGE (HUNDRED VOLT TO KILOVOLT), HIGH POWER DENSITY (>2 MW/CC), HIGH RADIATION ENVIRONMENT, HIGH SHOCK (UP TO A 1000GPEAK) AND VIBRATION (UP TO 60 GRMS) RESISTANCE, SAFE AND LONG CYCLE LIFE OF 1,000,000 CYCLES AT ROOM TEMPERATURE AND MORE THAN 100,000 CYCLES AT 400?C FOR FUTURE NASA SCIENTIFIC MISSION IN HARSH ENVIRONMENT. THE THIS CONTINUED DEVELOPMENT WILL FURTHER PROVE FEASIBILITY OF THIS TECHNOLOGY AND MOVE THE TECHNOLOGY FROM SPACE TRL LEVEL 3/4, DEMONSTRATED IN THE PHASE I, TO A TRL LEVEL 5/6 AT THE END OF THE PHASE II, WITH PARTS THAT COULD BE TESTED IN NASA ION THRUSTER PROPULSION DISCHARGE POWER SYSTEM (4 KW, 200 VDC AND 20 AMPS) BY THE END OF THE TWO-YEAR PHASE II IF AN APPLICABLE SYSTEM IS FOUND FOR TESTING.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
B: PURCHASE ORDER
IGF::OT::IGF THIS PHASE I SBIR CONTRACT WILL APPLY THE PRINCIPLES OF INTEGRATED MATERIALS COMPUTATIONAL ENGINEERING THE THE DESIGN AND FABRICATION OF A INTEGRAL THERMAL PROTECTION SYSTEM CYROGENIC STORAGE TANK. ANSYS MODELLING WILL BE CARRIED OUT TO SUB-OPTIMIZE THE MATERIALS PROPERTIES NECESSARY FOR AN INTEGRATED STRUCTURE-INSULATION-THERMAL PROTECTION SYSTEM USING MILTILAYERED THERMALLY INSULATING SYNTACTIC FOAMS CORE STRUCTURE. BY COMBINING STRUCTURAL AND INSULATION PERFORMANCE IN A HIGH TEMPERATURE STRUCTURE, A 65-100% REDUCTION IN PARASITIC THERMAL PROTECTION WEIGHT CAN BE ACHIEVED. MULTILAYER SANDWICH PANEL COUPONS WILL BE FABRICATED AND CHARACTERIZED FOR CRYOGENIC TO HIGH TEMPERATURE PROPERTIES AND THERMAL CYCLE RESPONSE TO VALIDATE THE MODEL, AND MANUFACTURING PATHFINDING EFFORTS WILL BE CONDUCTED FOR PRODUCTION OF CURVED MULTILAYERED SANDWICH PANELS. STRUCTURES.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
B: PURCHASE ORDER
IGF::OT::IGF THIS PHASE I SBIR CONTRACT WILL APPLY THE PRINCIPLES OF INTEGRATED MATERIALS COMPUTATIONAL ENGINEERING THE THE DESIGN AND FABRICATION OF A INTEGRAL THERMAL PROTECTION SYSTEM CYROGENIC STORAGE TANK. ANSYS MODELLING WILL BE CARRIED OUT TO SUB-OPTIMIZE THE MATERIALS PROPERTIES NECESSARY FOR AN INTEGRATED STRUCTURE-INSULATION-THERMAL PROTECTION SYSTEM USING MILTILAYERED THERMALLY INSULATING SYNTACTIC FOAMS CORE STRUCTURE. BY COMBINING STRUCTURAL AND INSULATION PERFORMANCE IN A HIGH TEMPERATURE STRUCTURE, A 65-100% REDUCTION IN PARASITIC THERMAL PROTECTION WEIGHT CAN BE ACHIEVED. MULTILAYER SANDWICH PANEL COUPONS WILL BE FABRICATED AND CHARACTERIZED FOR CRYOGENIC TO HIGH TEMPERATURE PROPERTIES AND THERMAL CYCLE RESPONSE TO VALIDATE THE MODEL, AND MANUFACTURING PATHFINDING EFFORTS WILL BE CONDUCTED FOR PRODUCTION OF CURVED MULTILAYERED SANDWICH PANELS. STRUCTURES.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
B: PURCHASE ORDER
IGF::OT::IGF NASA REQUIRES ADVANCED POWER ELECTRONIC AND ENERGY STORAGE DEVICES THAT CAN WORK AT VARIOUS TEMPERATURE (-100 DEGREE CELSIUS TO 400 DEGREE CELSIUS) AND HIGH OPERATING VOLTAGE WITH HIGH ENERGY AND POWER DENSITY WHERE TRADITIONAL POWER AND ENERGY STORAGE DEVICE CANNOT BE APPLIED. THE CURRENT STATE-OF-THE-ART OF THE CAPACITOR SUFFERS FROM TEMPERATURE RELIABILITY, ESPECIALLY AT HIGH TEMPERATURE, AS WELL AS LOW-ENERGY DENSITY, MAKING THEM BULKY AND COSTLY. POWER SYSTEMS FOR NASA MISSION MUST BE OPERATED EFFICIENTLY AT HIGH TEMPERATURES TO ELIMINATE THE NEED FOR ON BOARD COOLING SYSTEMS. THE HIGH PERFORMANCE CAPACITOR (TEMPERATURE RELIABILITY AND HIGH ENERGY DENSITY) WILL SAVE SPACE, REDUCE WEIGHT, AND IMPROVE RELIABILITY. THE PROPOSED PHASE I SBIR PROGRAM WILL DEMONSTRATE POWDERMET INC'S ABILITY TO PRODUCE AN ADVANCED NANOCOMPOSITE CAPACITOR CAN BE APPLIED IN HARSH AND EXTREME ENVIRONMENT AS REQUIRED BY NASA AEROSPACE EXPLORATION. THIS NOVEL CAPACITOR WILL FEATURE AS WIDE OPERATING TEMPERATURE (-100 DEGREE CELSIUS TO 400 DEGREE CELSIUS), HIGH OPERATING VOLTAGE (>KILOVOLT) AND HIGH-ENERGY DENSITY (>4 J/CC) AND HIGH POWDER DENSITY (>MW/CC) AS WELL AS OPERATING IN RADIATION ENVIRONMENT.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
DCA Definitive Contract
PROGRESS REPORT
AJ14: R&D- GENERAL SCIENCE/TECHNOLOGY: PHYSICAL SCIENCES (ENGINEERING DEVELOPMENT)
DCA Definitive Contract
IGF::OT::IGF REPLACING WORK CATEGORY "RESEARCH SCIENTIST" FROM DR. AARON LALONDE TO DR. HAIXIONG TANG
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
THE PURPOSE OF THIS MODIFICATION IS TO ADD INCREMENTAL FUNDING IN THE AMOUNT OF $551,592.36 FOR YEAR 2.
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
SBIR PH I; POWDERMET, INC.; ADMIN MOD TO CLARIFY LANGUAGE IN SECTION H-9.
AC61: R&D- DEFENSE SYSTEM: ELECTRONICS/COMMUNICATION EQUIPMENT (BASIC RESEARCH)
DCA Definitive Contract
N132-103 AWD
AC61: R&D- DEFENSE SYSTEM: ELECTRONICS/COMMUNICATION EQUIPMENT (BASIC RESEARCH)
DCA Definitive Contract
NOVEL ENERGETIC MATERIALS SBIR II
AB92: R&D- COMMUNITY SERVICE/DEVELOPMENT: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
IGF::OT::IGF PH II SBIR: NANODIELECTRICS FOR HIGH ENERGY DENSITY CAPACITORS
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
PROGRESS REPORT
AC61: R&D- DEFENSE SYSTEM: ELECTRONICS/COMMUNICATION EQUIPMENT (BASIC RESEARCH)
DCA Definitive Contract
TO CORRECT FUNDING DOCUMENTS. DE-OB FROM CLIN 0005 AND ADD CORRECT MONEY TO CLIN 006.
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
TO EXERCISE THE OPTION
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
INNOVATIVE HIGH STRENGTH NANOSTRUCTURED ALUMINUM-BASED COMPOSITES - 9 MONTH PERIOD OF PERFORMANCE EXTENSION AT NO ADDITIONAL COST TO THE GOVERNMENT
AE34: R&D- ECONOMIC GROWTH: MANUFACTURING TECHNOLOGY (ENGINEERING DEVELOPMENT)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
DCA Definitive Contract
PROGRESS REPORT
AE24: R&D- ECONOMIC GROWTH: PRODUCT/SERVICE IMPROVEMENT (ENGINEERING DEVELOPMENT)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
DCA Definitive Contract
RD
AC24: R&D- DEFENSE SYSTEM: MISSILE/SPACE SYSTEMS (ENGINEERING DEVELOPMENT)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
DCA Definitive Contract
SBIR PHASE 1 - NANOMATERIALS FOR THERMAL BATTERY
AC51: R&D- DEFENSE SYSTEM: WEAPONS (BASIC RESEARCH)
DCA Definitive Contract
TO CHANGE THE COR FROM CARLOS PEIERA TO CHUCK MCMULLEN AND THE PRINICPLE INVESTIGATOR FROM TIFFANY MILLER TO BRIAN DOUD.
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
DCA Definitive Contract
MODIFICATION TO CORRECT CLIN STRUCTURE FOR LINE ITEM 0002 FOR "INNOVATIVE HIGH STRENGTH NANOSTRUCTURED ALUMINUM-BASED COMPOSITES" FOR SMALL BUSINESS INNOVATIONS RESEARCH (SBIR) PHASE II.
AE34: R&D- ECONOMIC GROWTH: MANUFACTURING TECHNOLOGY (ENGINEERING DEVELOPMENT)
DCA Definitive Contract
INCREMENTAL FUNDING FOR YEAR 2 OF A PHASE II SMALL BUSINESS INNOVATION RESEARCH CONTRACT TITLED "INNOVATIVE HIGH STRENGTH NANOSTRUCTURED ALUMINUM BASED COMPOSITES".
AE34: R&D- ECONOMIC GROWTH: MANUFACTURING TECHNOLOGY (ENGINEERING DEVELOPMENT)
DCA Definitive Contract
POWDERMET INC PH I SBIR PROPOSAL: A113-119-0488 NANODIELECTRICS FOR HIGH ENERGY DENSITY CAPACITORS
AD92: R&D- DEFENSE OTHER: OTHER (APPLIED RESEARCH/EXPLORATORY DEVELOPMENT)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
DCA Definitive Contract
EXTEND THE PERIOD OF PERFORMANCE AT NO ADDITIONAL COST TO THE GOVERNMENT, AND TO MAKE OTHER ADMINISTRATIVE CHANGES.
AJ14: R&D- GENERAL SCIENCE/TECHNOLOGY: PHYSICAL SCIENCES (ENGINEERING DEVELOPMENT)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
PO Purchase Order
COMPOSITE ALUMINUM AIRCRAFT MATTING FOR HIGH-TEMPERATURE APPLICATIONS
AD91: OTHER DEFENSE (BASIC)
DCA Definitive Contract
SBIR PHASE II TOPIC AF083-244
AJ44: ENGINEERING (ENGINEERING)
DCA Definitive Contract
RD
AC21: R&D-MISSILE & SPACE SYS-B RES
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
DCA Definitive Contract
EXERCISE AN OPTION
AJ14: PHYSICAL SCIENCES (ENGINEERING)
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
D: DEFINITIVE CONTRACT
IN THIS PROPOSED PHASE II PROGRAM, BUILDS ON THE PHASE I FEAIBILITY WHERE A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WAS DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING IS HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. THE PHASE II PROGRAM WILL PROVIDE RADIATION MODELING AND TESTING FOR THESE NEW STRUCTURAL RADIATION SOLUTIONS AS WELL AS A PHYSICAL PROPERTY DATABASE FOR USING THEM IN SPACE HABITATS. THE PHASE II PROGRAM WILL ADDRESS ISSUES INCLUDING FLAMMABILITY, ATTACHMENT, AND INCORPORATION OF THESE NEW MATERIALS INTO EXISTING AND FUTURE SPACE HABITAT DESIGNS. THE ACCUMULATION OF THE PHASE II PROGRAM WILL BE PROTOTYPE COMPONENTS THAT CAN BE TESTED AT TRL LEVEL 5 OR FLOWN FOR TRL LEVEL 6.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
DCA Definitive Contract
PHASE I - SBIR
AD23: SERVICES (ADVANCED)
DCA Definitive Contract
PHASE II SBIR
AE34: R&D-MANUFACTURING TECH-ENG DEV
PO Purchase Order
THIS PROGRAM WILL MATURE AND FURTHER DEVELOP STRUCTURAL SYNTACTIC FOAM INSULATED INTEGRAL THERMAL PROTECTION SYSTEM (TPS) DESIGNS AND MATERIALS AS AN ENABLING TECHNOLOGY FOR THE HIGHLY RELIABLE, REUSABLE LAUNCH SYSTEM. THIS PROPOSED SBIR PROGRAM WILL BUILD ON POWDERMET'S EXTENSIVE PRIOR EXPERIENCE WITH SIC RIGID INSULATORS, CMCS, AND ULTRAHIGH-TEMPERATURE COATINGS, COMBINED WITH DESIGN MODELING FROM MR&D ASSOCIATES THAT IDENTIFIED POSITIVE DIRECTIONS NEEDED IN FOAM-SUPPORTED INTEGRAL STRUCTURAL TPS SYSTEMS.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
THIS PROPOSAL RELATES TO A NEW MATERIALS CONCEPT FOR AN ALUMINUM-CARBON NANOFIBER COMPOSITE, HIGH THERMAL CONDUCTIVITY ULTRA LIGHTWEIGHT MATERIAL THAT WILL FORM THE BASIS FOR ROBUST, LIGHTWEIGHT DEPLOYABLE METALLIC RADIATOR DESIGNS. SPECIFICALLY, THIS PROGRAM WILL RESULT IN AVAILABILITY OF HIGH THERMAL CONDUCTIVITY, LOW COEFFICIENT OF EXPANSION, EXTREMELY LOW DENSITY CARBON NANOTUBE-REINFORCED ALUMINUM COMPOSITES SUITABLE FOR USE IN RADIATOR PANEL FACESHEETS, CLOSEOUTS, SUPPORTS AND JOINTS.
AR11: R&D-AERO & SPACE TECH-B RES
DCA Definitive Contract
BONDING OF ULTRAHIGH STRENGTH ALLOYS
AD95: OTHER DEFENSE (OPERATIONAL)
DCA Definitive Contract
INCREMENTAL FUNDING
AJ14: PHYSICAL SCIENCES (ENGINEERING)
DCA Definitive Contract
THIS IS A MODIFICATION FOR A SIX (6) MONTH NO COST TIME EXTENSION, TO ALLOW THE CONTRACTOR TO FINISH TESTING AND DELIVERABLES TO INCLUDE A COPY OF THE REVISED DD254, REVISION NO. 4, AUTHORIZING THE CONTRACTOR TO RECEIVE AND GENERATE CLASSIFIED MATERIAL AND A COPY OF THE SECURITY CLASSIFICATION GUIDE FOR TACTICAL WHEELED VEHICLE ARMOR SYSTEMS.
AD21: SERVICES (BASIC)
DCA Definitive Contract
PHASE I - SBIR
AD23: SERVICES (ADVANCED)
DCA Definitive Contract
EXERCISE OF OTPION - PHASE I SBIR
AD92: OTHER DEFENSE (APPLIED/EXPLORATORY)
DCA Definitive Contract
SYNTH. TUGSTEN NANOPOWDERS / MODIFICATION TO BACK IN DCMA MOD WHICH DELETED AND ADDED CLAUSES
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
EXTENSION OF PERIOD OF PERFORMANCE FROM 24 JUN 2010 TO 24 AUG 2010.
AD21: SERVICES (BASIC)
PO Purchase Order
IN THIS PROPOSED PHASE I PROGRAM, A MULTIFUNCTIONAL LIGHTWEIGHT RADIATION SHIELD COMPOSITE WILL BE DEVELOPED AND FABRICATED. THIS STRUCTURAL RADIATION SHIELDING WILL BE A HIGH STRENGTH, SYNTACTIC POLYMERIC WHERE THE POLYMER IS FILLED WITH HIGH STRENGTH LOW Z MATERIAL. SPECIFICALLY, THIS PROGRAM WILL PRODUCE STRUCTURAL POLYMERIC ALUMINUM ALLOY-LIBH4 COMPOSITE MATERIALS LAYUPS. THESE STRUCTURAL COMPOSITES ARE DERIVED FROM SIMILAR STRUCTURES POWDERMET CURRENTLY PRODUCES USING HOLLOW SPHERES (LIGHTWEIGHT INSULATING STRUCTURES), AND MORE RECENTLY, ENERGETIC MATERIALS (SUCH AS KCLO4). THESE MATERIALS SERVE TO PROVIDE COMBINED STRUCTURAL PROPERTIES, THERMAL INSULATION, MASS-EFFICIENT RADIATION SHIELDING, AND COLLISION AND MICROMETEROID IMPACT ENERGY ADSORPTION.
AR11: R&D-AERO & SPACE TECH-B RES
DCA Definitive Contract
SBIR PHASE I
AD92: OTHER DEFENSE (APPLIED/EXPLORATORY)
DCA Definitive Contract
MODIFICATION TO EXTEND THE PERIOD OF PERFORMANCE AT NO COST TO THE GOVERNMENT
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
UPDATE WAWF CLAUSE AND THE GOVERNMENT POINTS OF CONTRACT IN SECTION G.
AJ14: PHYSICAL SCIENCES (ENGINEERING)
DCA Definitive Contract
PROGRESS REPORT
AJ14: PHYSICAL SCIENCES (ENGINEERING)
DCA Definitive Contract
PROGRESS REPORT
AJ14: PHYSICAL SCIENCES (ENGINEERING)
DCA Definitive Contract
PHASE II SBIR
AD21: SERVICES (BASIC)
DCA Definitive Contract
PHASE II SBIR
AD21: SERVICES (BASIC)
PO Purchase Order
SBIR PHASE I: TOPIC AF083-244 : POWDERMET INC.
AR11: R&D-AERO & SPACE TECH-B RES
PO Purchase Order
CERMET PLASMA SPRAY POWDERS
5850: VISIBLE INVISIBLE LIGHT COMMUN EQ
PO Purchase Order
CERMET PLASMA SPRAY POWDERS
5850: VISIBLE INVISIBLE LIGHT COMMUN EQ
DCA Definitive Contract
CONTRACT SUMMARY REPORT.
AC21: R&D-MISSILE & SPACE SYS-B RES
DCA Definitive Contract
"ADVANCED HIGH STRENGTH LOW WEIGHT ALUMINUM NANOFOAM ALLOYS"
AD92: OTHER DEFENSE (APPLIED/EXPLORATORY)
DCA Definitive Contract
MDA-SBIR PHASE I - BASIC EFFORT
AC23: R&D-MISSILE & SPACE SYS-ADV DEV
DCA Definitive Contract
NOVEL ENERGETIC MATERIALS SBIR II
AB92: R&D-OTHER SVC & DEVELOP-A RES/EXPL
DCA Definitive Contract
RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES
AD95: OTHER DEFENSE (OPERATIONAL)
DCA Definitive Contract
DELETE CLIN 0003
AC21: R&D-MISSILE & SPACE SYS-B RES
DCA Definitive Contract
PHASE II SBIR
AD21: SERVICES (BASIC)
DCA Definitive Contract
SYNTHESIZING TUGSTEN NANOPOWDERS
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
PHASE II
AD21: SERVICES (BASIC)
DCA Definitive Contract
SBIR PHASE I TOPIC N08-017
AC61: R&D-ELECTRONICS & COMM EQ-B RES
PO Purchase Order
RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
AD91: OTHER DEFENSE (BASIC)
DCA Definitive Contract
NO COST EXTENSION
AC21: R&D-MISSILE & SPACE SYS-B RES
PO Purchase Order
MODIFICATION TO CHANGE PAYMENT OFFICE
9630: ADDITIVE METAL MATERIALS
PO Purchase Order
POWDER
9630: ADDITIVE METAL MATERIALS
DCA Definitive Contract
SBIR PHASE I
AE24: R&D-PROD/SERV IMPROVEMENT-ENG DEV
DCA Definitive Contract
PHASE II SBIR
AD21: SERVICES (BASIC)
DCA Definitive Contract
SBIR PHASE II, TOPIC #:A05-047
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
ULTRA LIGHT-WEIGHT ENERGY ABSORBING ARMOR, SBIR PHASE II EFFORT.
AD21: SERVICES (BASIC)
DCA Definitive Contract
INCORPORATE SOW CHANGES
AC21: R&D-MISSILE & SPACE SYS-B RES
DCA Definitive Contract
WM-M EXERCISE OPTION OF NANOTUNGSTEN
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
NOVEL ENERGETIC MATERIALS SBIR II
AB92: R&D-OTHER SVC & DEVELOP-A RES/EXPL
DCA Definitive Contract
SBIR PHASE I TOPIC N07-004
AE24: R&D-PROD/SERV IMPROVEMENT-ENG DEV
DCA Definitive Contract
PHASE I SBIR OPTION.
AC41: DEFENSE TANK - AUTOMOTIVE (BASIC)
DCA Definitive Contract
NO-COST PERIOD OF PERFORMANCE EXTENSION WITH CONSIDERATIONS
AC21: R&D-MISSILE & SPACE SYS-B RES
PO Purchase Order
RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES
AD96: OTHER DEFENSE (MANAGEMENT/SUPPORT)
DCA Definitive Contract
BASIC EFFORT - PHASE I SBIR
AC23: R&D-MISSILE & SPACE SYS-ADV DEV
DCA Definitive Contract
NOVEL ENERGETIC MATERIALS SBIR II
AB92: R&D-OTHER SVC & DEVELOP-A RES/EXPL
DCA Definitive Contract
RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES
AD95: OTHER DEFENSE (OPERATIONAL)
PO Purchase Order
CONDUCT RESEARCH UNDER SBIR TOPIC
1040: CHEMICAL WEAPONS AND EQUIPMENT