A 30 cm mercury ion thruster module
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (4) , 420-423
- https://doi.org/10.2514/3.30295
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- A 30-cm, low-specific-impulse, hollow-cathode, mercury thrusterJournal of Spacecraft and Rockets, 1970
- Performance and control of a 30-cm-diam, low-impulse, Kaufman thrusterJournal of Spacecraft and Rockets, 1970
- SERT II - Durability of the hollow cathode and future applications of hollow cathodesJournal of Spacecraft and Rockets, 1970