Synonyms were used for: hot protection
Search without synonyms: title: Thermal protection systems and hot structures

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    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    David E Glass / Craig A Stephens | NTRS
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Thermal Protection Systems , hot structure

    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    David E Glass | NTRS
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Thermal Protection Systems, hot structure

    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    David E Glass | NTRS
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration

    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    David E Glass | NTRS
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration

    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    David E Glass | NTRS
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration

    Current Technology for Thermal Protection Systems

    Scotti, Stephen J. | NTRS | 1992
    capabilities in existing thermal protection systems in the Space Shuttle and in turbojet engines. This selection of 13 papers from NASA and industry ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Altitude Effects on Thermal Ice Protection System Performance; A Study of an Alternative Simulation Approach

    Addy, Gene / Wright, Bill / Orchard, David et al. | NTRS | 2015
    examined for ways to reduce energy consumption and to increase efficiency. A thermal ice protection systems must protect the aircraft from the ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Aircraft Design, Testing And Performance , thermal ice protection system

    Hypersonic Materials and Structures

    Glass, David E. | NTRS | 2016
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Fluid Mechanics And Thermodynamics

    Apollo experience report: Thermal protection from engine-plume environments

    Taylor, J. T. | NTRS | 1972
    Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are subjected to the impingement of hot ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Thermodynamics And Combustion

    Materials and Structures for Hypersonic Vehicles

    Darrel R Tenney / W Barry Lisagor / Sidney C Dixon | NTRS | 1989
    propulsion system, mission life requirements, and containment of liquid hydrogen. For hot-structures applications in the range from 600-1800°F ...
    Publisher: American Institute of Aeronautics and Astronautics
    Keywords: Thermal Protection System , Spacecraft Design, Testing and Performance

    Testing of DLR C/C-SiC for HIFiRE 8 Scramjet Combustor

    David E Glass / Diego P Capriotti / Thomas Reimer et al. | NTRS
    Ceramic Matrix Composites (CMCs) have been proposed for hot structures in scramjet combustors. Previous studies have calculated significant ...
    Publisher: NASA National Aeronautics and Space Administration

    ADEPT - A Mechanically Deployable Entry System Technology in Development at NASA

    Venkatapathy, Ethiraj / Wercinski, Paul / Cassell, Alan et al. | NTRS | 2016
    of the ground tests and design development completed to-date, and current plans for a small-scale flight test in the near future. ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Aerocapture Systems Analysis for a Neptune Mission

    Lockwood, Mary Kae / Edquist, Karl T. / Starr, Brett R. et al. | NTRS | 2006
    A Systems Analysis was completed to determine the feasibility, benefit and risk of an aeroshell aerocapture system for Neptune and to ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Ceramics and ceramic composites in future aeronautical and space systems

    Levine, Stanley R. | NTRS | 1992
    , spacecraft propulsion and power systems, aerospace (transatmospheric) vehicles, and space structures. Prototype component applications are evaluated ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Chemistry And Materials (General)

    Thermal characterization of reusable external insulation for the space shuttle.

    Brazel, J. P. / Tye, R. P. | NTRS | 1972
    Thermal protection systems utilizing reusable ceramic external insulations are under study for application to the orbiter vehicle of NASA's ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Thermodynamics And Combustion

    Structural design of integral tankage for advanced space transportation systems

    Macconochie, I. O. / Davis, R. B. / Lemessurier, R. W. | NTRS | 1982
    operate in a broad range of thermal environments while meeting requirements for low weight and reusability. Several approaches to integral tank ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    New Development Activities at NASA Ames in Reusable TPS Materials

    Adam Caldwell / Jay Feldman / Peter Marshall | NTRS
    reusable thermal protection systems (RTPS) that have not had broad application since the Space Shuttle era. Development of novel systems having a ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Reusable thermal protection materials

    New Development Activities at NASA Ames in Reusable TPS Materials

    Adam Caldwell / Jay Feldman / Peter Marshall | NTRS
    reusable thermal protection systems (RTPS) that have not had broad application since the Space Shuttle era. Development of novel systems having a ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Reusable thermal protection materials

    Graphene in the Sky and Beyond

    Siochi, Emilie J. | NTRS | 2014
    . Graphitized carbon and carbon/carbon composites are used in thermal protection systems and heat shields, carbon fiber composites in aircraft, and more ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Chemistry And Materials (General)

    Space Launch System Core Stage Green Run Base Heating: Anomaly, Mitigation and Flight Redesign

    Manish Mehta / Christopher I. Morris / Brandon L. Mobley et al. | NTRS
    was to confirm Core Stage tanking, propulsion and thrust vector control systems operations and performance to verify with predicted models ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Fluid Mechanics and Thermodynamics