Performance of a 15-centimeter diameter, hollow-cathode Kaufman thrustor
Author:
Affiliation:
1. NASA, LEWIS RESEARCH CENTER, CLEVELAND,OHIO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1968-88
Reference9 articles.
1. Mercury Cathodes for Ion Thrustors," QR-2 6. Readcr, P. D. "Durability Tcsts of Mcrcun. (NASA CR-81690), No". 1966, Hughes Rcscareh Ieclron-Ilombardent Ion 'llruslors, 1':qxr Labs., hhlibu, Calif. So. 66.231, hhr. 19GG, AmA, Xcw Yurk.
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1. SERT II - Mission, thruster performance, and in-flight thrust measurements;Journal of Spacecraft and Rockets;1971-03
2. A survey and evaluation of research on the discharge chamber plasma of Kaufman thrusters;Journal of Spacecraft and Rockets;1970-06
3. Langmuir probe measurements in a discharge from a hollow cathode;Journal of Spacecraft and Rockets;1970-04
4. Performance and control of a 30-cm-diam, low-impulse, Kaufman thruster;Journal of Spacecraft and Rockets;1970-01
5. SERT II - Thruster system ground testing;Journal of Spacecraft and Rockets;1970-01
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