Explore: Rocket Thrust

Discover books, insights, and more — all in one place.

Learn more about Rocket Thrust with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “rocket-thrust”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1High-power ion thruster technology

By

“High-power ion thruster technology” Metadata:

  • Title: ➤  High-power ion thruster technology
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

“High-power ion thruster technology” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1992
  • 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:

    Online Marketplaces

    Find High-power ion thruster technology at online marketplaces:


    2Multi-axis thrust measurements of the EO-1 pulsed plasma thruster

    By

    “Multi-axis thrust measurements of the EO-1 pulsed plasma thruster” Metadata:

    • Title: ➤  Multi-axis thrust measurements of the EO-1 pulsed plasma thruster
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

    “Multi-axis thrust measurements of the EO-1 pulsed plasma thruster” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • 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:

      Online Marketplaces

      Find Multi-axis thrust measurements of the EO-1 pulsed plasma thruster at online marketplaces:


      3Advanced tube-bundle rocket thrust chamber

      By

      “Advanced tube-bundle rocket thrust chamber” Metadata:

      • Title: ➤  Advanced tube-bundle rocket thrust chamber
      • Author:
      • Language: English
      • Number of Pages: Median: 12
      • Publisher: ➤  For sale by the National Technical Information Service - NASA
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

      “Advanced tube-bundle rocket thrust chamber” 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

      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:

        Online Marketplaces

        Find Advanced tube-bundle rocket thrust chamber at online marketplaces:


        4Theory and computation of optimal low- and medium-thrust orbit transfers

        By

        “Theory and computation of optimal low- and medium-thrust orbit transfers” Metadata:

        • Title: ➤  Theory and computation of optimal low- and medium-thrust orbit transfers
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, DC - Springfield, Va

        “Theory and computation of optimal low- and medium-thrust orbit transfers” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1996
        • 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:

          Online Marketplaces

          Find Theory and computation of optimal low- and medium-thrust orbit transfers at online marketplaces:


          5Test results of a 200W class hall thruster

          By

          “Test results of a 200W class hall thruster” Metadata:

          • Title: ➤  Test results of a 200W class hall thruster
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  [Cleveland, Ohio] - Springfield, Va

          “Test results of a 200W class hall thruster” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1999
          • 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:

            Online Marketplaces

            Find Test results of a 200W class hall thruster at online marketplaces:


            6Turbulence modelling of flow fields in thrust chambers

            By

            “Turbulence modelling of flow fields in thrust chambers” Metadata:

            • Title: ➤  Turbulence modelling of flow fields in thrust chambers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Research Institute, the University of Alabama in Huntsville
            • Publish Date:
            • Publish Location: ➤  [Washington, DC - Springfield, Va - [Huntsville, Ala.]

            “Turbulence modelling of flow fields in thrust chambers” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1993
            • 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:

              Online Marketplaces

              Find Turbulence modelling of flow fields in thrust chambers at online marketplaces:


              7The diagnostics of the external plasma for the plasma rocket

              By

              “The diagnostics of the external plasma for the plasma rocket” Metadata:

              • Title: ➤  The diagnostics of the external plasma for the plasma rocket
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - [Washington, DC

              “The diagnostics of the external plasma for the plasma rocket” 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.

              Online Borrowing:

                Online Marketplaces

                Find The diagnostics of the external plasma for the plasma rocket at online marketplaces:


                8Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)

                By

                “Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)” Metadata:

                • Title: ➤  Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - Engineering Experiment Station, Auburn University - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  [Washington, DC - Springfield, Va - Auburn, Ala

                “Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five)” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1980
                • 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:

                  Online Marketplaces

                  Find Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) at online marketplaces:


                  9A performance comparison of two small rocket nozzles

                  By

                  “A performance comparison of two small rocket nozzles” Metadata:

                  • Title: ➤  A performance comparison of two small rocket nozzles
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                  “A performance comparison of two small rocket nozzles” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1996
                  • 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:

                    Online Marketplaces

                    Find A performance comparison of two small rocket nozzles at online marketplaces:


                    10A life comparison of tube and channel cooling passages for thrust chambers

                    By

                    “A life comparison of tube and channel cooling passages for thrust chambers” Metadata:

                    • Title: ➤  A life comparison of tube and channel cooling passages for thrust chambers
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  Washington, DC - [Springfield, Va

                    “A life comparison of tube and channel cooling passages for thrust chambers” 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

                    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:

                      Online Marketplaces

                      Find A life comparison of tube and channel cooling passages for thrust chambers at online marketplaces:



                      Wiki

                      Source: Wikipedia

                      Wikipedia Results

                      Search Results from Wikipedia

                      Rocket

                      without using any surrounding air. A rocket engine produces thrust by reaction to exhaust expelled at high speed. Rocket engines work entirely from propellant

                      Thrust-to-weight ratio

                      among others, jet engines, rocket engines, pump-jets, Hall-effect thrusters, and ion thrusters – all of which generate thrust by expelling mass (propellant)

                      Thrust vectoring

                      Thrust vectoring, also known as thrust vector control (TVC), is the ability of an aircraft, rocket or other vehicle to manipulate the direction of the

                      Rocket engine

                      A rocket engine is a reaction engine, producing thrust in accordance with Newton's third law by ejecting reaction mass rearward, usually a high-speed jet

                      Rocket engine nozzle

                      pressure is higher than the exit pressure, it decreases the net thrust produced by the rocket, which can be seen through a force-balance analysis. If ambient

                      Thrust

                      propelling jet of a jet engine, or by ejecting hot gases from a rocket engine. Reverse thrust can be generated to aid braking after landing by reversing the

                      Dual-thrust rocket motor

                      In a dual-thrust solid propellant rocket engine, the propellant mass is composed of two different types (densities) of fuel. In the case of a tandem dual-thrust

                      Orion (rocket)

                      American sounding rocket. The Orion has a length of 5.60 meters, a diameter of 0.35 m, a launch weight of 400 kg, a launch thrust of 7 kN and a ceiling

                      Rocket propellant

                      Rocket propellant is used as a reaction mass ejected from a rocket engine to produce thrust. The energy required can either come from the propellants

                      Solid rocket booster

                      A solid rocket booster (SRB) is a solid propellant motor used to provide thrust in spacecraft launches from initial launch through the first ascent. Many