Award Data

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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

  1. WAVELENGTH DIPLEXED, FIBER COUPLED, COHERENT LASER RADAR MEASUREMENT SYSTEM

    SBC: DIGITAL SIGNAL CORP.            Topic: N/A

    N/A

    SBIR Phase I 1990 National Aeronautics and Space Administration
  2. Vortex Flap Improvements for Enhanced Low-Speed Aerodynamics of Supersonic-Cruise Aircraft

    SBC: VIGYAN, INC.            Topic: N/A

    Leading edge vortex flap modifications are proposed for improvedlow-speed lift and L/D characteristics of supersonic cruiseaircraft. The aim is to increase the vortex-lift potential inaddition to generating vortex thrust on highly-swept wingconfigura

    SBIR Phase I 1994 National Aeronautics and Space Administration
  3. Very-Long-Baseline-Array Recorder Applied to High-Resolution Nicrowave Survey Data

    SBC: Interferometrics, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
  4. Turn-Key Approach to Optimal Control via Differential Inclusion

    SBC: ANALYTICAL MECHANICS ASSOCIATES, INC.            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
  5. TUNABLE SOLID-STATE UV FREQUENCY CONVERTER FOR OZONE DIAL INSTRUMENTATION

    SBC: FIBERTEK, INC.            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration
  6. Transistion Control in Corner Flow of a Supersonic Square Nozzle

    SBC: High Technology Corporation            Topic: N/A

    "Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section

    SBIR Phase I 1994 National Aeronautics and Space Administration
  7. Thin-Film Pressure Sensor with Optical Output

    SBC: Gre, Inc.            Topic: N/A

    We propose a thin, flexible pressure sensing film with optical out- put consisting of a polymer LED on a piezoelectric polymer substrate. The innovation lies in combining these two types of polymers to make a single sensor which will provide a minimal intrusion method for measuring pressure distributions on structures in free-flight and/or wind tunnel tests. Spatial resolution should be better tha ...

    SBIR Phase I 1994 National Aeronautics and Space Administration
  8. Test, Control, and Monitoring System Wireless Information Network

    SBC: SENTEL CORPORATION            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
  9. Supersonic Jet-Noise Prediction and Control

    SBC: High Technology Corporation            Topic: N/A

    N/A

    SBIR Phase I 1994 National Aeronautics and Space Administration
  10. SPACECRAFT OPERATIONAL AUTONOMOUS REASONING SYSTEM (SOARS)

    SBC: Scientific Simulation Inc            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration
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