Evolution and status of the 30-cm engineering model ion thruster

Author:

MASEK T.1,POESCHEL R.1,COLLETT C.1,SCHNELKER D.1

Affiliation:

1. HughesResearch Laboratories, Malibu, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Reference27 articles.

1. H. J. King, et a l . "Low Voltage 3 0 - c m Ion T h r u s t e r . " NASA CR-120919. F e b r u a r y ,

2. u 1972.

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1. Application of Ion Thrusters to High-Thrust, High-Specifi c-Impulse Nuclear Electric Missions;Nuclear Space Power and Propulsion Systems;2008-08-22

2. Origin of the electron-bombardment ion thruster;Journal of Spacecraft and Rockets;1981-07

3. Ion Propulsion Cost Effectivity;Electric Propulsion and Its Applications to Space Missions;1981-01-01

4. Characteristics of the LeRC/Hughes J-Series 30-cm Engineering Model Thruster;Electric Propulsion and Its Applications to Space Missions;1981-01-01

5. Ion beam divergence characteristics of two-grid accelerator systems;AIAA Journal;1978-05

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