Award Data

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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 June, 2020.

  1. A COUPLED JET EMBEDDING AND EULERIAN-LAGRANGIAN APPROACH TO SIMULATE REACTIVE FLUID MECHANICS IN LIQUID ROCKET ENGINES

    SBC: Cham Of North America Inc            Topic: N/A

    AN ANALYTICAL MODEL AND A COMPUTER CODE FOR THE DETAILED SIMULATION OF THREE-PHASE FLOWS IN LIQUID ROCKET THRUST CHAMBERS IS PROPOSED. THE MODEL DESCRIBES BEHAVIOR OF THE LIQUID, DISPERSED AND GASEOUS PHASES IN A MOST EFFICIENT FORM. THE CONTINOUS GAS-PHASE FLOW AND COMBUSTION ARE DESCRIBED IN EULERIAN COORDINATES; THE SPRAY FLOW, DROPLET EVAPORATION AND COMBUSTION PROCESSES ARE SIMULATED IN A GRI ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
  2. A RELIABLE, MECHANICAL CRYOCOOLER FOR 80 K COOLING IN SPACE

    SBC: Alabama Cryogenic Engineering, Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  3. Advanced Aerodynamic Analysis For Propulsion Airframe Integration

    SBC: Research In Flight, LLC            Topic: A105

    Research in Flight is proposing to develop a fundamentally new, lower order, high fidelity solution approach for the aerodynamic analysis required for engine integration studies. This new approach is based on a new tool known as Flightstream. Flightstream is a surface vorticity based solver which uses an unstructured surface geometry, and a correlation for skin friction which is based on the sur ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  4. Advanced Zirconium Carbide Tie-Tubes for NTP

    SBC: Plasma Processes, LLC            Topic: H202

    Nuclear Thermal Propulsion (NTP) has been identified as a critical technology needed for human missions to Mars due to its increased specific impulse (Isp) as compared to traditional chemical propulsion systems. To achieve this high Isp, NTP reactors must operate at extremely high temperatures (i.e., >2400K) for long periods of time. However, many of the best materials for some reactor component ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  5. Advanced Flow Control System for In-Space Electric Propulsion

    SBC: CU AEROSPACE L.L.C.            Topic: T2

    CU Aerospace (CUA) and the University of Michigan (UM) propose the development of the Cycle Automated Mass Flow (CAMFlow) system for reliable and well-regulated flow control. CAMFlow uses an innovative control scheme that enables stable operation using only Boolean valve states, even for the low flow rates necessary for sub-kilowatt Hall effect thrusters. This methodology removes system complexity ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  6. Advanced Plasma Sprayed Conductive Thermal Control Material Systems (TCMS)- For Improved Performance

    SBC: APPLIED MATERIAL SYSTEMS ENGINEERING, INC.            Topic: S3

    This Phase I proposal is submitted to verify the materials and process engineering of the space environment stable, multifunctional Plasma Sprayable conductive thermal control material system (TCMS) that can be applied to space hardware and can enables the hardware to carry higher leakage current through co doping process engineering for the high electrical conductivity. An innovative space enviro ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
  7. AERODYNAMIC HEATING UPGRADE OF THE PARABOLIZED NAVIER-STOKES(PNS) CODE

    SBC: Remtech Inc.            Topic: N/A

    N/A

    SBIR Phase I 1985 National Aeronautics and Space Administration
  8. AEROHEATING FLIGHT INSTRUMENTATION

    SBC: Remtech Inc.            Topic: N/A

    N/A

    SBIR Phase I 1987 National Aeronautics and Space Administration
  9. Air Vehicle Gust Response analysis for Conceptual Design

    SBC: Research In Flight, LLC            Topic: T15

    Research in Flight (RIF) and Auburn University are offering the development of an advanced, robust tool and methodology that allows the simulation and modeling of gust and wake vortex encounters for Distributed Electric Propulsion (DEP) enabled Urban Air Mobility (UAM) vehicle concepts. DEP enabled UAM concepts offer the potential for large performance improvements by exploiting favorable synergie ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  10. AN IMPROVED TOXIC VAPOR DETECTOR FOR HYDRAZINE MONOMETHYLHYDRAZINE AND HC1

    SBC: Transducer Research Inc.            Topic: N/A

    AN ALL SOLID-STATE MICRO-ELECTROCATALYTIC AMPEROMETRIC SENSOR IS PROPOSED FOR THE DETECTION, IDENTIFICATION, AND QUANTIFICATION OF HYDRAZINE, MONOMETHYLHYDRAZINS AND HC1. DURING PHASE I, SEVERAL INNOVATIVE SENSORS ARE CONSTRUCTED AND EVALUATED. THE SENSORS USE SOLID IONIC CONDUCTORS AS THE ELECTROLYTE. IMPROVEMENTS IN SENSOR RELIABILITY ARE ACHIEVED BY USING THESOLID-STATE APPROACH. IMPROVEMENTS I ...

    SBIR Phase I 1987 National Aeronautics and Space Administration
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