Colloid Thrustor Beam Analysis PDF Download
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Author: Carl T. Norgren
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ISBN:
Category : Electrostatic accelerators
Languages : en
Pages : 52
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Author: Carl T. Norgren
Publisher:
ISBN:
Category : Electrostatic accelerators
Languages : en
Pages : 52
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Book Description
Author: Carl T. Norgren
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Author:
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ISBN:
Category :
Languages : en
Pages : 216
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Author: Ronald J. Schertler
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ISBN:
Category : Electrostatic accelerators
Languages : en
Pages : 28
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1576
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 970
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
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Author: Jerrell Maurice Turner
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Category : Space vehicles
Languages : en
Pages : 63
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An experimental program established that a multiple needed colloid thruster produces a beam with anisotropic current, specific charge, and mass flow distributions as a function of beam half-angle. Data reduction and analysis indicated that the assumptions of beam isotropy yields valid relative performance but the absolute value of performance determined from the time-of-flight spectrometer is questionable. A segmented time-of-flight collector, consisting of ten electrically isolated rings which could be connected to simulate a total collector, was the primary diagnostic tool. For thrust, specific impulse, and efficiency, results from the segmented and total collector differed by up to 30%. Even larger differences were observed in the case of mass flow. By moving the collector, it was found that the distance between the source and time-of-flight collector has a significant effect on specific charge and current. (Author).
Author:
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Category : Aeronautics
Languages : en
Pages : 612
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