Charged Particle Electrostatic Thrusters.
Abstract
This program was directed toward the demonstration of long-term efficient electrostatic engine operation in the 1000-second specific impulse range. The state of the art in this performance range has been advanced to where practical flight system design is feasible. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1969
- Accession Number
- AD0849510
Entities
People
- Marshall N. Huberman
- Philip W. Kidd
Organizations
- TRW Inc.