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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

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Displaying 204571 - 204580 of 207712 results
  1. A SOLID STATE AUTONOMOUS ICE PROTECTION SYSTEM FOR ALL-WEATHER RPV'S

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INCREASED PERFORMANCE DEMANDS BEING MADE ON RPV'S WILL SOON REQUIRE AN ALL-WEATHER ICE PROTECTION CAPABILITY. THE OBJECT OF OUR STUDY WILL BE TO APPLY UNIQUE ICING SENSOR AND ICE PROTECTION TECHNOLOGIES WHICH WERE DEVELOPED BY INNOVATIVE DYNAMICS (IDC) UNDER A RECENT NASA SBIR CONTRACT. WE HAVE SUCCESSFULLY DEICED A RPV TYPE WING SECTION LEADING EDGE DURING PRELIMINARY TESTS PERFORMED WITHIN OUR I ...

    SBIR Phase I 1987 Department of DefenseDefense Advanced Research Projects Agency
  2. INVESTIGATION ON DETECTION OF TRANSITIONING FLOWFIELDS

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    THE OBJECTIVE OF THIS PROGRAM IS TO DEVELOP AND FLIGHT TEST A UNIQUE MEASUREMENT SYSTEM THAT WILL PASSIVELY SENSE LAMINAR, TRANSITIONAL, AND TURBULENT BOUNDARY LAYER FLOW. THIS ADVANCED AERODYNAMIC FLOW SENSOR DESIGN INCORPORATES A THIN, SOLID-STATE POLYMER FILM THAT SENSES BOTH NORMAL AND SHEAR BOUNDARY LAYER FORCES. PRELIMINARY TESTS OF AN EIGHT SEGMENT SENSOR ARRAY POSITIONED ON THE WING OF A G ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  3. AIRCRAFT ICING PERFORMANCE MEASUREMENT SYSTEM EXPERIMENTAL INVESTIGATION ON THE DETECTION OF TRANSITIONING

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INNOVATIVE DYNAMICS IS PROPOSING A UNIQUE SOLID-STATE, LOW-COST, RUGGED ICE DETECTION SYSTEM TO REDUCE THE HAZARDS OF AIRCRAFT ICING. THIS SYSTEM WILL SENSE AN IMPENDING AIRCRAFT WING STALL CONDITION BY DIRECTLY MEASURING THE INTENSITY OF TURBULENT AIRFLOW INDUCED BY ICE ACCRETION. THE KEY SYSTEM COMPONENTS ARE PIEZOELECTRIC TRANSDUCERS FOR SENSING BOUNDARY LAYER PRESSURE FLUCTUATIONS AND A MICROC ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  4. LASER-ACOUSTIC SYSTEM FOR VERTICAL PROFILING BURIED AND SURFACE ICE

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INNOVATIVE DYNAMICS PLANS TO INVESTIGATE SOLID-STATE LASERS TO BE INCORPORATED IN A LASER-ACOUSTIC SYSTEM FOR REMOTE SENSING APPLICATIONS IN THE ARCTIC ENVIRONMENT. THIS SYSTEMCONSISTS OF A PULSED LASER TRANSMITTER AND AN ACOUSTIC RECEIVER, BOTH OPERATED IN THE AIR. THE LASER BEAM IS FOCUSED TO A SMALL SPOT ON THE SURFACE OF THE GROUND. STRONG ABSORPTION OF THE LASER ENERGY AT THE SURFACE LIMITS P ...

    SBIR Phase I 1989 National Science Foundation
  5. LOW COST ANGLE-OF-ATTACK SENSOR FOR SUBSONIC AIRCRAFT

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    THE OBJECTIVE OF THIS PROJECT IS TO DEVELOP A LOW COST SMARTANGLE OF ATTACK AND ANGLE OF SIDESLIP SENSOR (SAASS) THAT RESOLVES AERODYNAMIC FLOW FORCES EXERTED ON A SPHERE ELEMENTINTO COMPONENTS OF MAGNITUDE AND DIRECTION. THIS CONCEPT UTILIZES A UNIQUE 3-AXIS FORCE TRANSDUCER DESIGNED TO BE RUGGED, SENSITIVE, AND MOTIONLESS. THE PROPOSED DESIGN HAS A FIXED-POSITION SENSING ELEMENT CAPABLE OF MEASU ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  6. AIRCRAFT HEALTH MONITORING SYSTEM

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    THE COMPANY HAS DEVELOPED A UNIQUE, THIN-FILM SENSOR DESIGN THAT WHEN INTEGRATED WITH A STRUCTURAL MEMBER COULD DETECT FATIQUE CRACKS, CORROSION, AND ICE ACCRETION AS WELL AS EXTERNAL PRESSURE VARIATIONS INDICATIVE OF AN IMPENDING WINGSTALL. THESE SENSORS AND SIGNAL PROCESSING SOFTWARE CAN BE INTEGRATED INTO AN ADVANCED HEALTH MONITORING SYSTEM (HMS) TO EXTEND SIGNIFICANTLY THE LIFE SPAN OF THE AG ...

    SBIR Phase II 1991 National Aeronautics and Space Administration
  7. DEMONSTRATION OF NEURAL NETWORK PERFORMANCE FOR ON-LINE HEALTH MONITORING AND INSPECTION OF AIRCRAFT

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INNOVATIVE DYNAMICS IS PROPOSING TO IMPLEMENT NEURAL NETWORK SIGNAL PROCESSING SOFTWARE WITH OUR AIRCRAFT HEALTH MONITORING SYSTEM (HMS) TESTBED. HMS IS A UNIQUE DISTRIBUTED SYSTEM BASED ON "SMART STRUCTURES" TECHNOLOGY. IT HAS RECENTLY SUCCESSFULLY COMPLETED A FLIGHT TEST PROGRAM AT NASA LEWIS THAT DEMONSTRATED THE FEASIBILITY TO DETECT RIVET LINE CORROSION AND LEADING EDGE ICE ACCRETION. BY MONI ...

    SBIR Phase II 1992 Department of DefenseNavy
  8. AN INVESTIGATION OF SMART SKIN TECHNOLOGY FOR VORTEX FLOW DETECTION

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INNOVATIVE METHODS FOR MEASURING AND CONTROLLING VORTEX DOMINATED FLOWS MUST BE DEVELOPED TO ACHIEVE ENHANCED MISSION PERFORMANCE OF ADVANCED TECHNOLOGY FIGHTERS. THE PRIMARY OBJECTIVE OF THE PROPOSED RESEARCH IS TO DEFINE AND EXPERIMENTALLY QUANTIFY TECHNIQUES FOR MEASURING SURFACE FLOW PATTERNS AND VORTEX STRUCTURES. THE INITIAL PHASE I EFFORT WILL DEMONSTRATE AN INNOVATIVE CONCEPT BASED ON "SMA ...

    SBIR Phase I 1992 National Aeronautics and Space Administration
  9. ICE PROTECTION TECHNOLOGY DEMONSTRATION FOR UAVS

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    OVER THE PAST FIVE YEARS, A RESEARCH CONSORTIUM SPONSORED BY THE NASA LEWIS RESEARCH CENTER HAS BEEN THE SOURCE OF THE DEVELOPMENT OF SEVERAL NEW ICE PROTECTION TECHNOLOGIES DIRECTLY APPLICABLE TO UNMANNED AUTONOMOUS VEHICLES (UAV'S). INNOVATIVE DYNAMICS (ID) HAS BEEN INVOLVED IN SEVERAL OF THESE PROGRAMS AND AS A RESULT HAS DEVELOPED AN ICE SENSOR BASED ON "SMART STRUCTURES" TECHNOLOGY. BY MONITO ...

    SBIR Phase II 1994 Department of DefenseDefense Advanced Research Projects Agency
  10. SHAPE MEMORY ALLOYS FOR USE IN ROTORCRAFT DEICING SYSTEMS

    SBC: INNOVATIVE DYNAMICS INC.            Topic: N/A

    INCREASED READINESS AND SAFETY DEMANDS BEING MADE ON HELICOPTERS REQUIRE AN ALL-WEATHER CAPABILITY. WHILE SEVERAL PROMISING DE-ICERS HAVE BEEN DEVELOPED FOR FIXED WING AIRCRAFT, THE REQUIREMENT STILL EXISTS FOR A RELIABLE DE-ICING SYSTEM COMPATIBLE WITH HELICOPTER BLADES. THE IDEAL DE-ICER MUST BE SMALL, REQUIRE A MINIMUM AMOUNT OF INTERFACE HARDWARE, AND BE ABLE TO OPERATE EFFICIENTLY ON LOW POWE ...

    SBIR Phase II 1992 National Aeronautics and Space Administration
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