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Source: The Open Library

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1Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine

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“Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine” Metadata:

  • Title: ➤  Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine
  • Author:
  • Language: English
  • Number of Pages: Median: 21
  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - [Springfield, VA

“Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1989
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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    2Thrust augmentation measurements using a pulse detonation engine ejector

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    “Thrust augmentation measurements using a pulse detonation engine ejector” Metadata:

    • Title: ➤  Thrust augmentation measurements using a pulse detonation engine ejector
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor - Available from NASA Center for Aerospace Information
    • Publish Date:
    • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA - Hanover, MD

    “Thrust augmentation measurements using a pulse detonation engine ejector” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2003
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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      3A numerical study of chemically reacting flow in nozzles

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      “A numerical study of chemically reacting flow in nozzles” Metadata:

      • Title: ➤  A numerical study of chemically reacting flow in nozzles
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

      “A numerical study of chemically reacting flow in nozzles” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1989
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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        4Operating characteristics of the Russian D-55 thruster with anode layer

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        “Operating characteristics of the Russian D-55 thruster with anode layer” Metadata:

        • Title: ➤  Operating characteristics of the Russian D-55 thruster with anode layer
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Operating characteristics of the Russian D-55 thruster with anode layer” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1994
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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          5A data acquisition and storage system for the ion auxiliary propulsion system cyclic thruster test

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          “A data acquisition and storage system for the ion auxiliary propulsion system cyclic thruster test” Metadata:

          • Title: ➤  A data acquisition and storage system for the ion auxiliary propulsion system cyclic thruster test
          • Author:
          • Language: English
          • Publisher: ➤  For sale by the National Technical Information Service - NASA
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

          “A data acquisition and storage system for the ion auxiliary propulsion system cyclic thruster test” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1989
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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            6RHETT/EPDM performance characterization

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            “RHETT/EPDM performance characterization” Metadata:

            • Title: ➤  RHETT/EPDM performance characterization
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
            • Publish Date:
            • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio]

            “RHETT/EPDM performance characterization” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1998
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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              7Evaluation of various thrust calibration techniques on an F404 engine

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              “Evaluation of various thrust calibration techniques on an F404 engine” Metadata:

              • Title: ➤  Evaluation of various thrust calibration techniques on an F404 engine
              • Author:
              • Number of Pages: Median: 26
              • Publisher: ➤  Ames Research Center, Dryden Flight Research Facility
              • Publish Date:
              • Publish Location: Edwards, Calif

              “Evaluation of various thrust calibration techniques on an F404 engine” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1990
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              8High pressure, earth storable rocket technology

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              “High pressure, earth storable rocket technology” Metadata:

              • Title: ➤  High pressure, earth storable rocket technology
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration] - National Technical Information Service [distributor
              • Publish Date:
              • Publish Location: ➤  [Washington, D.C - Springfield, VA

              “High pressure, earth storable rocket technology” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1997
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                9Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

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                “Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Metadata:

                • Title: ➤  Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
                • Publish Date:
                • Publish Location: ➤  [Cleveland, Ohio] - [Hanover, Md

                “Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2003
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                Online Borrowing:

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