SERT II - Design requirements for integrating electric propulsion into a spacecraft
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (3) , 209-213
- https://doi.org/10.2514/3.30249
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Review of SERT II power conditioningJournal of Spacecraft and Rockets, 1971
- SERT II - Mission, thruster performance, and in-flight thrust measurementsJournal of Spacecraft and Rockets, 1971
- Electrical Breakdown between Metal Electrodes in High Vacuum. I. TheoryJournal of Applied Physics, 1967