Transient and Steady Performance of an Ion Rocket Thrust Augmentor Final Report
1966
130 pages
Report
No indication
English
Electric & Ion Propulsion , Electron emission , Heat transfer , Ionic propulsion , Langmuir probe , Pirani gauge , Accelerator , Augmentation , Beam , Cylinder , Electron , Emission , Ion , Ionic , Measurement , Performance , Porosity , Pressure , Propulsion , Rocket , Secondary , Thrust , Tungsten
Thrust augmentor inlet optimization
AIAA | 1986
|NTIS | 1971
|Reversed Cowl Flap Inlet Thrust Augmentor
NTIS | 1975
|