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

    D. E. Glass | NTIS | 2021
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Publisher: National Aeronautics and Space Administration, Washington, DC.
    Keywords: Hot structure , Thermal protection systems

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

      D. E. Glass | NTIS | 2021
      Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...

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

      D. E. Glass | NTIS | 2023
      Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
      Publisher: National Aeronautics and Space Administration, Washington, DC.

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

      D. E. Glass | NTIS | 2021
      Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
      Publisher: National Aeronautics and Space Administration, Washington, DC.

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

      D. E. Glass | NTIS | 2008
      Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
      Keywords: Thermal protection , Hot surfaces , Thermal resistance

    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

    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
    Keywords: Thermal Protection Systems, hot structure

    European Directions for Hypersonic Thermal Protection Systems and Hot Structures

    Glass, David E. | NTRS | 2007
    This presentation will overview European Thermal Protection Systems (TPS) and Hot Structures activities in Europe. The Europeans have a lot ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

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

    Glass, David E. | NTRS | 2008
    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

    Integrated Thermal Protection Systems and Heat Resistant Structures

    Pichon, Thierry / Lacoste, Marc / Barreteau, R. et al. | NTRS | 2006
    heath management system and the high temperature structures testing, and NASA Langley led the insulation characterization. Though the task was ...
    Publisher: NASA National Aeronautics and Space Administration

      Integrated Thermal Protection Systems and Heat Resistant Structures

      Pichon, Thierry / Lacoste, Marc / Glass, David E. | NTRS | 2006
      & Technology program to develop integrated thermal protection systems and heat resistant structures for reentry vehicles. Due to changes within NASA's ...
      Publisher: NASA National Aeronautics and Space Administration
      Keywords: Spacecraft Design, Testing And Performance

    Mars 2020 Thermal Protection Systems Sizing and Development

    Robin A S Beck / Milad Mahzari / Joseph D Williams | NTRS
    . The approach used in sizing the thermal protection systems (TPS) for the various components of the MSL spacecraft included ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Thermal protection systems

    Technology - Structures and thermal protection systems

    Anderson, R. A. | NTRS | 1970
    Space shuttle structural design and thermal protection systems ...
    Publisher: NASA National Aeronautics and Space Administration

    NASA Efforts to Explore Additively Manufactured Thermal Protection Systems

    Ethiraj Venkatapathy / Stanley A Bouslog / Adam Sidor | NTRS
    Development of the thermal protection system (TPS) needed to protect external and internal surfaces during launch, ascent, cruise, and ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Chemistry And Materials (General) , Spacecraft Design, Testing And Performance

    NASA Efforts to Explore Additively Manufactured Thermal Protection Systems

    E. Venkatapathy / S. A. Bouslog / A. Sidor | NTIS | 2022
    Development of the thermal protection system (TPS) needed to protect external and internal surfaces during launch, ascent, cruise, and ...
    Publisher: National Aeronautics and Space Administration, Washington, DC.

    Caravan with freeze protection and improved thermal efficiency

    Free access
    KIM JONG BURM | European Patent Office | 2021

    Disclosed is a caravan with improved freeze protection and thermal efficiency. The disclosed caravan with improved freeze protection and

     ...

    Methods and systems for detecting leakage in a thermal protection apparatus using a liquid crystal sheet

    Free access
    DE PAU-JR ROBERT / SILJEE DAVID V | European Patent Office | 2021

    In an example, method of inspecting a thermal protection apparatus is described. The apparatus comprises a composite wall and a thermal

     ...

    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

    Pyrolytic materials for thermal protection systems

    Garber, A.M. | Engineering Index Backfile | 1963
    Characteristics of pyrolytic or refractory anisotropic materials, with emphasis on pyrolytic graphite for design and missile and re-entry ...

    Thermal protection systems for all-weather reusable launch vehicles

    Giegerich, Marc J. | NTRS | 1993
    The topics addressed are: (1) thermal protection system technology needs; and (2) long-term, reusable thermal protection materials, such as ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Evaluation of coated columbium for thermal protection systems application

    Rummler, D. R. / Black, W. E. | NTRS | 1975
    Coated columbium alloys were evaluated for thermal protection system (TPS) application in the maximum operating temperature range from 1370 ...
    Publisher: NASA National Aeronautics and Space Administration

    Evaluation of columbium alloy thermal protection systems for space shuttle.

    Black, W. E. / Rummler, D. R. | NTRS | 1973
    Publisher: NASA National Aeronautics and Space Administration