The design and performance of a versatile ion thruster simulator-Reference-Cited by-同舟云学术

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The design and performance of a versatile ion thruster simulator

Published:1975-03-19 Issue: Volume: Page:
ISSN:
Container-title:11th Electric Propulsion Conference
language:
Short-container-title:

Author:

PYE J.¹

Affiliation:

1. Royal Aircraft Establishment, Farnborough, Hants., England

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1975-383

Reference13 articles.

1. "Some dynamic characteristics of an electronbombardment ion thruster," NASA TN D-4204 (1967) 3. P . A . Mueller and E.V. Pavlik, "Control analysis

2. research on the discharge chamber plasma oi a Kaufman thruster." AIM paper 69-494 (1969).

3. cathode investigations at the Royal Aircraft Establishment." AIM paper 73-1137 (1973). 6 . J.S. Serafini and F.F. Terdan, "Plasma

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