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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

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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:

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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:

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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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                  Find Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility at online marketplaces:



                  Wiki

                  Source: Wikipedia

                  Wikipedia Results

                  Search Results from Wikipedia

                  EmDrive

                  NASA observed a small apparent thrust from one such test, however subsequent studies suggested this was a measurement error caused by thermal gradients

                  Pound (force)

                  (symbol: lbf, sometimes lbf,) is a unit of force used in some systems of measurement, including English Engineering units and the foot–pound–second system

                  Megathrust earthquake

                  forced underneath another. The earthquakes are caused by slip along the thrust fault that forms the contact between the two plates. These interplate earthquakes

                  Burpee (exercise)

                  The burpee, a squat thrust with an additional stand between repetitions, is a full body exercise used in strength training. The movement itself is primarily

                  Full Thrust

                  Full Thrust is a science fiction strategy wargame written by Jon Tuffley and published by Ground Zero Games of England. It is usually played with miniature

                  Rocket engine test facility

                  bottoms of the fuel tanks. The effect of the propellant weight on the thrust measurement system (TMS) must be accounted for as the engine is firing. The rocket

                  Magnetic sail

                  Hagiwara, T.; Kajimura, Y.; Oshio, Y.; Funaki, I. (July 4–10, 2015). "Thrust Measurement of Magneto Plasma Sail with Magnetic Nozzle by Using Thermal Plasma

                  Blind thrust earthquake

                  A blind thrust earthquake occurs along a thrust fault that does not show signs on the Earth's surface, hence the designation "blind". Such faults, being

                  Test Stand VII

                  The tower included an elevator and a German-made Toledo scale for thrust measurements. Actual launches were from a steel table-like structure (firing stand

                  SERT-1

                  Description and Operation of spacecraft in SERT-1 ion thrustor flight test Results from SERT-1 ion rocket flight test Thrust measurement of SERT-1 ion thrustors