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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. Thermal Management System for Long-Lived Venus Landers

    SBC: Advanced Cooling Technologies, Inc.            Topic: S303

    Long-lived Venus landers require power and cooling. Heat from the roughly 64 General Purpose Heat Source (GPHS) modules must be delivered to the convertor with minimal ÄT. The cooling system must be shutoff during the transit to Venus without overheating the GPHS modules. This program will develop an alkali metal Variable Conductance Heat Pipe (VCHP) integrated with a two-phase heat collection/tr ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  2. Loop Heat Pipe with Thermal Control Valve for Passive Variable Thermal Link

    SBC: Advanced Cooling Technologies, Inc.            Topic: S302

    Loop heat pipes (LHPs) can provide variable thermal conductance needed to maintain electronics and batteries on Lunar/Martian rovers/landers within desired temperature range. During lunar day, the LHP transfers the heat to the radiator for rejection. During the fourteen-day-long lunar night, the sink temperature drops, lowering LHP and WEB/battery temperatures. Without a variable thermal link, the ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  3. Interfacial Design of Composite Ablative Materials

    SBC: Advanced Cooling Technologies, Inc.            Topic: A201

    This Phase I Small Business Innovative Research project proposes to develop a multiscale computational methodology capable of accurate prediction of the properties and performance of insulating ablative materials that are used to protect the re-entry of vehicles from excessive thermal loads. In particular, this effort will focus on multi-million atom, reactive molecular dynamics (MD) simulations o ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  4. A Compact, Efficient Pyrolysis/Oxidation System for Solid Waste Resource Recovery in Space

    SBC: Advanced Fuel Research, Inc.            Topic: X203

    Pyrolysis processing can be used in near term missions for volume reduction, water recovery (drying), stabilization, and enhanced water and oxygen recovery through thermochemical reactions. For longer term missions, the added benefits include production of fuel, multi-purpose carbon, and reactants for in-situ resource utilization (ISRU). The objective of the Phase I SBIR program was to demonstrate ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  5. A Fast-Response Atmospheric Turbulence (FRAT) Probe with Gas-Sampling Ducts

    SBC: AEROPROBE CORPORATION            Topic: S1

    Aeroprobe proposes to design, construct and test an air-data probe with substantially higher frequency response than currently available. This fast-response atmospheric turbulence probe (FRAT probe) will be able to sample ambient air, and measure CO2 and other gases. Phase I work demonstrated that with a proper design of the probe nose, ingestion holes for gas sampling do not interfere with port ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  6. Integration of Performance Based Operations into ATM and TFM Simulations

    SBC: Aerotech Research            Topic: A3

    FAA predicts that air traffic will double or even triple by 2025 and unless solutions that enable improvements in the use of airspace can be developed and implemented, significant airspace congestion will occur. Advancements in aircraft capabilities via new technologies can enable aircraft to operate more efficiently in the NAS and to operate safely in areas previously restricted. AeroTech propo ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  7. In Situ Wake Vortex Encounter Detection and Reporting System

    SBC: Aerotech Research            Topic: A3

    Wake vortices are a critical constraint to aircraft separation and therefore airportal throughput, which is already at or near capacity at many major airports in the NAS. Improvements to current methods of spacing aircraft could significantly increase airportal capacity, but there is currently limited awareness of wake encounters and information with which to assess spacing in real-time or to desi ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  8. Desensitized Optimal Filtering and Sensor Fusion Tool Kit

    SBC: ANALYTICAL MECHANICS ASSOCIATES, INC.            Topic: O404

    It is proposed to develop desensitized optimal filtering techniques and to implement these algorithms in a navigation and sensor fusion tool kit. These proposed desensitized optimal filtering techniques include recent advances in robust and/or adaptive generalized Kalman and Sigma-Point filters for non-Gaussian problems with uncertain error statistics, as well as a proposed new technique to desen ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  9. Crack Closure Based Self Healing Process for Metallic Structures

    SBC: ANALYTICAL SERVICES & MATERIALS, INC.            Topic: A113

    Analytical Services and Materials, Inc. (AS&M) is proposing to develop and validate a process that can extend the fatigue life of and potentially self-heal existing fatigue damage of aluminum and titanium alloys. The genesis of the proposed process is research conducted at the NASA Langley Research Center that developed a low melting point coating that flows into the crack when activated. The fa ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  10. Frequency Up-Conversion Detection System with Single Photon Sensitivity within 1-1.8 ¿m and 3-4 ¿m for ASCENDS Mission: A Novel Approach to Lidar

    SBC: ArkLight            Topic: S101

    PI at ArkLight proposes a novel approach to photon counting detectors at near-IR (1-1.8 µm) and mid-IR (3-4 µm) with single photon sensitivity, representing an innovative Lidar technology for ASCENDS mission. She will convert the input signals at 1.27 µm and 1.57 µm to those at 579 nm and 634 nm, respectively, within a periodically-poled LiNbO3 wafer, pumped by a Nd:YAG laser at 1.064 µm or a ...

    SBIR Phase I 2010 National Aeronautics and Space Administration

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