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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. THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO PROVIDE THE DESIGNER OF AN TI-RADIATION HOMING MISSILES WITH THE INFORMATION NECESSARY TO STRUCTURE FUTURE STUDIES AND TECHNOLOGY PROGRAMS AIMED AT DEVELOPING AN ANTI- RADIATION MISSILE CAPABLE OF HOMING ON

    SBC: Cas Inc.            Topic: N/A

    THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO PROVIDE THE DESIGNER OF AN TI-RADIATION HOMING MISSILES WITH THE INFORMATION NECESSARY TO STRUCTURE FUTURE STUDIES AND TECHNOLOGY PROGRAMS AIMED AT DEVELOPING AN ANTI- RADIATION MISSILE CAPABLE OF HOMING ON THREAT RADIATION MISSILE CAPABLE OF HOMING THREAT RADARS UTILIZING SPREAD SPECTRUM TECHNIQUES. THIS INVOLVES THE FOLLOWING TWO TASKS: 1. DEFINE THE C ...

    SBIR Phase I 1983 Department of DefenseAir Force
  2. IMPROVEMENTS, MAINTENANCE AND REFURBISHMENT

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

    THIS RESEARCH ADDRESSES TECHNIQUES AND MATERIALS FOR ON-ORBIT MAINTENANCE AND REFURBISHMENT OF THERMAL CONTROL SURFACE COATINGS USED ON LONG-LIFE SPACECRAFT. IN MANY CASES, CONSERVATIVE ASSUMPTIONS ON THE EFFECTS OF LONG-TERM DEGRADATION HAVE DRIVEN THE DESIGN OF SPACECRAFT THERMAL SYSTEMS TOWARD OVER CAPACITY WHICH RESULTS IN WEIGHT, SIZE, COMPLEXITY, AND COST PENALTIES. IF CRITICAL SURFACES COUL ...

    SBIR Phase I 1983 Department of DefenseAir Force
  3. RESEARCH ON LARGE, HIGHLY ACCURATE INFLATABLE REFLECTORS

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

    N/A

    SBIR Phase I 1983 Department of DefenseAir Force
  4. Fiber Optic Raman Sensors for the Remote Determination of Composite Chemical Characteristics

    SBC: ADVANCED PROCESSING TECHNOLOGY, INC.            Topic: N/A

    N/A

    SBIR Phase I 1994 Department of DefenseAir Force
  5. AN INNOVATIVE AIR-TURBO ROCKER (ATR) SCRAMJET PROPULSION SYS AND SUPPORTING DESIGN APPROACH

    SBC: CFD Research Corporation            Topic: N/A

    Development of combined Air-Turbo-Rocket(ATC/Scramjet component technology suitable for numerous USAF propulsion missions is proposed. Preliminary component design will focus on attaining fully throttleable boost and sustain thrust, vehicle speeds from Mach 0 to 8, and range as required. Activities during Phase I include: (1) Generator of an ATR/Scramjet system and component analysis methodology b ...

    SBIR Phase II 1994 Department of DefenseAir Force
  6. Monorotor for Air Turborocket (ATR) Engine

    SBC: CFD Research Corporation            Topic: N/A

    N/A

    SBIR Phase I 1994 Department of DefenseAir Force
  7. Advantages of Two-Phase Switched Reluctance Machines for More Electric Aircraft Power Generation

    SBC: ISOTHERMAL SYSTEMS RESEARCH            Topic: N/A

    The current development of an electric power generation system for the More Electric Aircraft (MEA) is based on a low-risk extension of existing three-phase, switched reluctance machine (SRM) technology. This research program proposes to study an alternate two-phase SRM and its associated power-conditioning converter. By the nature of the proposed machine, it has 50% of its stator coils active at ...

    SBIR Phase I 1994 Department of DefenseAir Force
  8. Innovative Control Effectors for Hypersonic Vehicles

    SBC: DYNETICS, INC.            Topic: N/A

    Dynetics proposes to initiate a study to investigate the potential benefits of applying a lattice control surface technology to hypersonic vehicles as a means to improve aircraft performance and operating efficiency. Under the Phase I effert, Dynetics will develop preliminary designs of generic lattice control surface concepts suitable for use on various types of hypersonic vehicles. Dynetics will ...

    SBIR Phase I 1994 Department of DefenseAir Force
  9. Flight Control Science and Technology

    SBC: DYNETICS, INC.            Topic: N/A

    Dynetics proposes to initiate study to investigate the potential benefits of applying lattice control surface technology to transport aircraft as a means to substantially improve aircraft performance and operating efficiency. Under the Phase I effort, Dynetics will develop preliminary designs of generic lattice control surfaces concepts suitable for use on various types of transport aircraft. Dyne ...

    SBIR Phase I 1994 Department of DefenseAir Force
  10. P-Version Finite Element Method for the Compressible Navier-Stokes Equations with and without Body Force

    SBC: Encom, Inc.            Topic: N/A

    This proposal is concerned with the accurate computer simulation of compressible transonic and supersonic flows. It explores the feasibility of developing a Computational Fluid Dynamics (CFD) code based on the p-version of the finite element method, which alleviates some of the inherent limitations and difficulties of established finite difference/finite volume methods for such flows. Numerical di ...

    SBIR Phase I 1994 Department of DefenseAir Force

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