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The Award database is continually updated throughout the year. As a result, data for the given year is not complete until April of the following year. Annual Reports data is a snapshot of agency reported information for that year and hence might look different from the live data in the Awards Information charts.

  1. A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    This proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration into a new Combined Cycle Engine with Ramjets. The concept is an intermittent combustion jet engine that harnesses travelling detonation waves to accomplish compression and chemical reaction. The goal ...

    SBIR Phase I 1993 Department of DefenseAir Force
  2. A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    An innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereby reducing cooling requirements and aircraft weight while improving engine performance. Specifically, CONvective and TRANspiration cooling (CONTRAN) are uniquely combined, relying on hydrogen coolant ...

    SBIR Phase I 1993 Department of DefenseAir Force
  3. Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine

    SBC: Advanced Projects Research, Incorporated            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  4. Instrumentation for Non-Intrusive Water Droplet Size and Mass Flux Measurements Utilizing the Phase Doppler Method

    SBC: Aerometrics Inc.            Topic: N/A

    There is a need for non-intrusive instrumentation to characterize the drop size distribution and volume flux in support of on-line engine/inlet icing tests. The ducts may vary from three to twelve feet in diameter with flow field speeds from Mach 0.2 to 0.5. The Phase Doppler technique offers the best potential for making these measurements non-intrusively and with sufficient accuracy to meet the ...

    SBIR Phase I 1993 Department of DefenseAir Force
  5. Characterization of Simulated Weather Environments In Aerospace Ground Test Cells.

    SBC: Aerometrics Inc.            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force
  6. INFLATABLE SMART MISSILE WING DESIGN EVALUATION

    SBC: AEROTECH ENGINEERING & RESEARCH CORP.            Topic: N/A

    THREE AREAS OF ACTIVE MISSILE WING RESEARCH WILL BE PURSUED. THE FIRST SECTION WILL EVALUATE THE MATERIALS TO BE USED IN THE INFLATABLE WING SPARS, RIBS, SKINS, PRESSURE BLADDERS AND ACTIVE ELEMENTS. SPECIMENS OF HIGH ORTHOGONALITY COMPOSITES (POLYURETHANE-GRAPHITE) WILL BE CONSTRUCTED ALONG WITH SAMPLE ISOTROPIC BLADDER MATERIALS (MYLAR OR TEFLON) SO THAT THEIR FUNDAMENTAL PROPERTIES CAN BE EVALU ...

    SBIR Phase II 1993 Department of DefenseAir Force
  7. Application Specific Electronic Design Synthesis

    SBC: Akm Associates, Inc.            Topic: N/A

    The Air Force and other DoD organizations are continuously developing new electronic components for their weapons and other systems. In this effort they are in need of tools to aid in the automated design, or synthesis, of these components. One component of particular importance is the computer processor. It is of enough importance that the Air Force has established a standard for this device (MIL ...

    SBIR Phase I 1993 Department of DefenseAir Force
  8. Robust Nonlinear Autopilot Designs for HAVE DASH II Missiles

    SBC: AMERICAN GNC CORPORATION            Topic: N/A

    The nonlinearity and unceitainty inherent in the HAVE DASH II missile's dynamics have been a great challenge to the autopilot design that is required to have satisfactory performance for all flight conditions in probable engagements. Several advanced robust nonlinear approaches, namely, inversion-based control laws, analytical gain scheduling, and nonlinear servo-regulator are proposed to design a ...

    SBIR Phase I 1993 Department of DefenseAir Force
  9. Integrated Fire Control/Weapon System Design and Evaluation for Internetted Applications

    SBC: AMERICAN GNC CORPORATION            Topic: N/A

    The integrated fire control/weapon system design is an important part of the general effort in integrated avionics, flight control, fire control, and weapon systems design to improve weapon effectiveness and aircraft survivability. The delivery accuracy can be improved through reducing the effects of significant error sources in targeting, fire control, and weapon systems. The increase in survivab ...

    SBIR Phase I 1993 Department of DefenseAir Force
  10. Autonomous Navigation with Passive Imaging Sensors

    SBC: AMERICAN GNC CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1993 Department of DefenseAir Force

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