Exhaust Measurements on the Plasma from a Pulsed Coaxial Gun

Author:

ASHBY D.E.T.F.1,GOODING T. J.1,HAYWORTH B. R.1,LARSON A.V.1

Affiliation:

1. General Dynamics/Astronautics, San Diego, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference10 articles.

1. Presented as Preprint 64-705 at AIAA Fourth Electric Propulsion Conference, Philadelphia, Pa., August 31-September2,1964; revision received January 14, 1965. This work was supported by NASA on Contract No. NAS3-2594.

2. Longmire, C. L. "The use of plasma for propulsion of interplanetary rockets," pp.3-11; Starr,W. L.and Naff, J. T. "Acceleration of metal-derived plasmas," pp. 47-59; Marshall, J. "Hydromagnetic plasma gun," pp. 60-72; Gartenhaus, S. and Tannenwald, L. M. "Propulsion from pinch collapse," pp. 73-78, Plasma Acceleration, edited byS. W. Kash (Stanford Univ. Press, Stanford, Calif.1960).

3. An energy inventory in a coaxial plasma accelerator driven by a pulse line energy source

4. DIAGNOSTIC STUDIES OF A PINCH PLASMA ACCELERATOR

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