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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. Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center

    SBC: ACCUDYNE SYSTEMS, INC.            Topic: A404

    Reduced-mass polymer composite materials are crucial to the success of aerospace systems for reducing vehicle weight. But, composite material adoption is inhibited because the autoclave consolidation required is prohibitively expensive for the large tanks and skins contemplated in the Next Generation Launch Technology (NGLT) Program. To remedy this, NASA-LaRC has been developing cost-effective, ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  2. Optimal Composite Materials using NASA Resins or POSS Nanoparticle Modifications for Low Cost Fabrication of Large Composite Aerospace Structures

    SBC: ACCUDYNE SYSTEMS, INC.            Topic: X602

    Reduced mass composite materials are crucial to the success of aerospace systems, but their adoption is inhibited because they require autoclave consolidation, a process that is prohibitively expensive for large aerospace structure. To remedy this, NASA-LaRC has been developing cost-effective high-performance thermoplastic composite processing equipment that enables out-of-autoclave tape placemen ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  3. Novel Long-Term CO2 Removal System

    SBC: COMPACT MEMBRANE SYSTEMS, INC.            Topic: B301

    Current Technology for CO2 removal from enclosed air of spacecraft utilizes LiOH canisters for CO2 absorption. This absorption is irreversible so longer flights require more LiOH. For long duration flights it is essential that a small, lightweight system that recovers the CO2 be developed. This allows the CO2 to be used to regenerate O2 for re-use. Compact Membrane systems (CMS) has identified ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  4. Multidisciplinary Design Under Uncertainty for Entry Vehicles

    SBC: MICHIGAN ENGINEERING SERVICES LLC            Topic: X802

    The physical difficulty of designing entry vehicles originates from the large degree of coupling between the various disciplines involved in the design. Every subsystem design decision has far reaching consequences that must be evaluated in a multidisciplinary fashion in order to assess the impact on the weight and the performance of the entire vehicle. The disciplines which must be accounted an ...

    SBIR Phase I 2005 National Aeronautics and Space Administration

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