• DocumentCode
    386909
  • Title

    Placing the satellite in its orbit

  • Author

    Rosen, Mark

  • Author_Institution
    Naval Research Laboratory, Washington, DC, USA
  • Volume
    4
  • fYear
    1966
  • fDate
    21-25 March 1966
  • Firstpage
    103
  • Lastpage
    107
  • Abstract
    The VANGUARD satellite launching vehicle is a three-stage rocket of which the first two stages are guided and the third stage is maintained in a fixed orientation while it is firing. The first stage, an improved Viking, serves primarily to raise the remaining stages to altitude. The second stage, another liquid-propellant rocket, contains the guidance for the three-stage vehicle and, in addition, supplies some of the propulsive energy. The third stage, a solid-propellant rocket, is ejected from the second stage at orbital altitude and provides about half of the required orbital velocity. The VANGUARD launching vehicle system was chosen from a number of possible two- and three-stage vehicle combinations. It represents the smallest satellite launching vehicle consistent with the present state of rocket development.
  • Keywords
    Earth; Helium; Inductors; Kinetic energy; Navigation; Propulsion; Rockets; Satellite broadcasting; Skin; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    1958 IRE International Convention Record
  • Conference_Location
    New York, NY, USA
  • Type

    conf

  • DOI
    10.1109/IRECON.1956.1150453
  • Filename
    1150453