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Maximum propellant utilization in an electron-bombardment thruster
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1971 |
| Description | Maximum propellant utilization in electron bombardment ion thrusters using mercury for propellant |
| File Size | 675715 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710026637 |
| Archival Resource Key | ark:/13960/t1wd8mj0x |
| Language | English |
| Publisher Date | 1971-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |