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  • Books
  • Other Sources  (2)
  • SPACECRAFT PROPULSION AND POWER  (2)
  • 1980-1984  (2)
  • 1982  (2)
  • 1
    Publication Date: 2019-07-13
    Description: A rail accelerator was chosen for study as an electromagnetic space propulsion device because of its simplicity and existing technology base. The results of a mission feasibility study using a large rail accelerator for direct launch of ton-size payloads from the Earth's surface to space, and the results of initial tests with a small, laboratory rail accelerator are presented. The laboratory rail accelerator has a bore of 3 by 3 mm and has accelerated 60 mg projectiles to velocities of 300 to 1000 m/s. Rail materials of Cu, W, and Mo were tested for efficiency and erosion rate.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA-TM-83015 , E-1449 , NAS 1.15:83015 , AIAA PAPER 82-1938 , Intern. Electric Propulsion Conf; Nov 17, 1982 - Nov 19, 1982; New Orleans
    Format: application/pdf
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  • 2
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: (Previously announced in STAR as N83-12143)
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: AIAA PAPER 82-1938 , Japan Society for Aeronautical and Space Sciences, and DGLR, International Electric Propulsion Conference; Nov 17, 1982 - Nov 19, 1982; New Orleans, LA
    Format: text
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