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Source: The Open Library

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1Mission advantages of constant power, variable ISP electrostatic thrusters

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“Mission advantages of constant power, variable ISP electrostatic thrusters” Metadata:

  • Title: ➤  Mission advantages of constant power, variable ISP electrostatic thrusters
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
  • Publish Date:
  • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA

“Mission advantages of constant power, variable ISP electrostatic thrusters” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2000
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    2Sample mission application of capacitor powered hall thrusters

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    “Sample mission application of capacitor powered hall thrusters” Metadata:

    • Title: ➤  Sample mission application of capacitor powered hall thrusters
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C - Springfield, Va

    “Sample mission application of capacitor powered hall thrusters” 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 Sample mission application of capacitor powered hall thrusters at online marketplaces:



      Wiki

      Source: Wikipedia

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      Ion thruster

      mass savings of electric propulsion, predicted its use in spacecraft propulsion and attitude control, and advocated electrostatic acceleration of charged

      Field-emission electric propulsion

      Field-emission electric propulsion (FEEP) is an advanced electrostatic space propulsion concept, a form of ion thruster, that uses a liquid metal as a

      Spacecraft electric propulsion

      Spacecraft electric propulsion (or just electric propulsion) is a type of spacecraft propulsion technique that uses electrostatic or electromagnetic fields

      Ion-propelled aircraft

      driven air thrusters. Electrostatic Antigravity on NASA's "Common Errors in propulsion" page NASA: Asymmetrical Capacitors for Propulsion DeFelice, David.

      Gridded ion thruster

      low-thrust spacecraft propulsion method running on electrical power by using high-voltage grid electrodes to accelerate ions with electrostatic forces. The ion

      Fusor

      and L. W. Jameson, "Inertial-Electrostatic Propulsion Spectrum: Airbreathing to Interstellar Flight", Journal of Propulsion and Power, v 11, no 2. The authors

      Spacecraft propulsion

      Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites. In-space propulsion exclusively deals with propulsion systems

      Fusion rocket

      A fusion rocket is a theoretical design for a rocket driven by fusion propulsion that could provide efficient and sustained acceleration in space without

      Ion wind

      wind or electric wind is the airflow of charged particles induced by electrostatic forces linked to corona discharge arising at the tips of some sharp

      Nuclear thermal rocket

      that store energy internally. NTRs have been proposed as a spacecraft propulsion technology, with the earliest ground tests occurring in 1955. The United