List

For best search results, use the search terms first and then apply the filters
Reset

The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. 5 NS ECL MEMORY MODULE USING POLYLITHICS MULTICHIP MODULES (MCM)

    SBC: Polylithics Inc            Topic: N/A

    THE THIN FILM INTERCONNECT DESIGNED AND MANUFACTURED BY POLYLITHICS ALLOWS EXTREMELY TIGHT PACKAGING OF BARE INTEGRATED CIRCUIT DIE. DUE TO SHORT WIRE LENGTHS AND A CONTROLLED ELECTRICAL ENVIRONMENT, SIGNALS TRAVEL EFFICIENTLY BETWEEN CHIPS. WITH CHIP TO CHIP COMMUNICATION BOTTLENECKS ELIMINATED, POLYLITHICS MULTICHIP CIRCUITS OFFER DISTINCT PERFORMANCE ADVANTAGED OVER CONVENTIONAL PRINTED CIRCUIT ...

    SBIR Phase I 1990 Department of DefenseAir Force
  2. A BALLISTIC RANGE EXPERIMENT TO MEASURE ELECTRON DENSITY PROFILES WITH HOLOGRAPHIC INTERFEROMETRY

    SBC: PHYSICAL RESEARCH, INC.            Topic: N/A

    THE INNOVATIVE PROPOSED HEREIN CONCERNS THE DEVELOPMENT OF A HOLOGRAPHIC DIAGNOSTIC TECHNIQUE FOR THE MEASUREMENT OF ELECTRON DENSITY PROFILES IN THE FLOWS OVER A RV BALLISTIC RANGE MODEL. AN EXPERIMENT IS IDENTIFIED IN WHICH HOLOGRAPHIC PLASMA MEASUREMENTS WILL BE USED FOR REFINEMENT AND VALIDATION OF COMPUTATIONAL FLOW/CHEMISTRY ANALYSIS. THE TECHNICAL APPROACH IS BASED ON THE DEVELOPMENT OF A T ...

    SBIR Phase I 1990 Department of DefenseAir Force
  3. A COMPUTATIONAL MODEL FOR THRUST REVERSING AND VECTORED JETS

    SBC: NIELSEN ENGINEERING & RESEARCH, INC.            Topic: N/A

    BECAUSE OF RECENTLY DEFINED TACTICAL THREATS IT IS DESIRABLE TO IMPROVE THE MANEUVERABILITY AND TAKE-OFF/LANDING ASPECTS OF AIRCRAFT PERFORMANCE. IT HAS BEEN DETERMINED THAT SUCH IMPROVEMENTS CAN BE ACCOMPLISHED BY THE USE OF THRUST REVERSERS OR VECTORED JETS. IN ORDER TO DESIGN AIRCRAFT SATISFACTORILY IT IS NECESSARY TO HAVE A PREDICTION METHOD THAT IS SUFFICIENTLY ACCURATE. THE MOST DIFFICULT FL ...

    SBIR Phase II 1990 Department of DefenseAir Force
  4. A HIGH PERFORMANCE LAPTOP OPTIMAL PLANNING WORKSTATION

    SBC: Mimd Systems, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  5. A LIGHT CURING FUEL TANK REPAIR SEALANT

    SBC: Pda Engineering            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  6. A TWO-STREAM PLASMA ELECTRON MICROWAVE SOURCE FOR HIGH POWER MILLIMETER WAVE GENERATION

    SBC: Applied Microwave Plasma            Topic: N/A

    A NOVEL HIGH POWER MILLIMETER/MICROWAVE SOURCE IS PROPOSED IN WHICH TWO INTERPENETRATING STREAMS OF ELECTRONS, FLOWING THROUGH A BACKGROUND PLASMA IN A STATIC MAGNETIC FIELD ARE USED TO GENERATE A HOT-ELECTRON PLASMA THAT IS CONFINED IN A MIRROR-LIKE MAGNETIC FIELD IN THE FORM OF A FOLDED-CUSP MAGNETIC CONFIGURATION. ENERGY STORED IN THE ANISOTROPIC, HOT-ELECTRON PLASMA IS THEN USED TO AMPLIFY UNS ...

    SBIR Phase II 1990 Department of DefenseAir Force
  7. ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

    SBC: HYPERSONICS            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  8. ADVANCED METHODS FOR ATMOSPHERIC MODELING

    SBC: NIELSEN ENGINEERING & RESEARCH, INC.            Topic: N/A

    ATMOSPHERIC SCIENCE INVOLVES STUDIES OF VERY COMPLEX PHYSICAL PROCESSES. OFTEN, SIMPLIFIED VERSIONS OF THESE PROCESSES ARE SIMULATED IN A LABORATORY OR ON A COMPUTER. COMPUTATIONAL FLUID DYNAMICS (CFD) METHODS PROVIDE A GOOD WAY TO PERFORM THESE SIMULATIONS OF ATMOSPHERIC PHENOMENA, SINCE THEY ALLOW FOR THE EASY VARIATION OF INDEPENDENT VARIABLES. HOWEVER, AS THE NUMBER OF POSSIBLE COMBINATIONS OF ...

    SBIR Phase I 1990 Department of DefenseAir Force
  9. ADVANCED SUSPENSION SYSTEM FOR SIMULATING ON-ORBIT CONDITIONS

    SBC: CSA Engineering, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1990 Department of DefenseAir Force
  10. AERODYNAMIC ANALYSIS OF SUBSONIC VERTICAL TAKE-OFF AND LANDING AIR VEHICLE

    SBC: Corpdray Research Inc.            Topic: N/A

    THE ADVENT OF THE CORDRAY ROTARY ENGINE HAS MADE POSSIBLE SUBSTANTIAL INCREASES IN THE POWER TO WEIGHT RATIO AVAILABLE TO THE AIRCRAFT DESIGNER. ENGINE SELECTION IS HISTORICALLY THE PRIMARY DETERMINATIVE OFVEHICLE DESIGN AND PERFORMANCE. THE AVAILABILITY OF THIS ENGINE ALONGWITH ADVANCES IN COMMAND AND CONTROL ELECTRONICS MAKES POSSIBLE A NEW CLASS OF VEHICLE CAPABLE OF VERTICAL TAKE OFF AND THEN ...

    SBIR Phase II 1990 Department of DefenseAir Force

Agency Micro-sites

SBA logo
Department of Agriculture logo
Department of Commerce logo
Department of Defense logo
Department of Education logo
Department of Energy logo
Department of Health and Human Services logo
Department of Homeland Security logo
Department of Transportation logo
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government