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    Rail accelerators for space transportation: An experimental investigation (1986)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An experimental program was conducted at the Lewis Research Center with the objective of investigating the technical feasibility of rail accelerators for propulsion applications. Single-stage, plasma driven rail accelerators of small (4 by 6 mm) and medium (12.5 by 12.5 mm) bores were tested at peak accelerating currents of 50 to 450 kA. Streak-camera photography was used to provide a qualitative description of plasma armature acceleration. The effects of plasma blowby and varying bore pressure on the behavior of plasma armatures were studied.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA-TP-2571 , E-2754 , NAS 1.60:2571
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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