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Magneto-plasma-dynamic arc thruster
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1973 |
| Description | The performance of a magnetoplasmadynamic arc thruster, in the 600 to 2,100 seconds specific impulse range, was improved by locating its cathode in the exhaust beam downstream of the anode and main propellant injection point. |
| File Size | 907612 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730017033 |
| Archival Resource Key | ark:/13960/t6rz41m8s |
| Language | English |
| Publisher Date | 1973-05-29 |
| Access Restriction | Open |
| Subject Keyword | Arc Jet Engines Rocket Engines Plasma Engines Magnetohydrodynamic Flow Performance Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |