| 摘要 |
A gas flow from a gas reservoir is accelerated up to supersonic velocity beyond the throat of a Laval nozzle. The accelerated supersonic gas flow is introduced into a plasma generating preaccelerating system, and thereby converted into the plasma flow of the velocity close to the thermal's. Then, the primary plasma flow is introduced into an arcjet discharger, to be accelerated to super thermal velocity by the viscosity force, similar to a sonic wind.
|
