Vacuum cathode arc-induced pulsed thruster
A vacuum cathode arc-induced pulsed thruster includes a housing where a triggering room and an electric discharging room are defined and are in communication with each other, a first anode unit and a first cathode unit concentrically disposed in the triggering room, a second anode unit disposed in the electric discharging room, an insulating fuel layer concentrically located between the first anode unit and the first cathode unit, a main insulating layer concentrically surrounded by the first cathode unit, and a second cathode unit inserted from the triggering room into the electric discharging room. Thus, the vacuum cathode arc-induced pulse thruster is lightweight and has low manufacturing costs, low system complexity, and less energy consumption. Carbon deposition caused during an electric discharging process is prevented from affecting an inducing effect to thereby prolong the service life of the thruster and increase the control precision and inducing precision effectively.
1. A vacuum cathode arc-induced pulsed thruster comprising:
a housing defining a central axis and having an inner peripheral wall, with a triggering room and an electric discharging room respectively enclosed by said inner peripheral wall, said triggering room and said electric discharging room being in communication with each other;
a first anode unit and a second anode unit respectively disposed in said triggering room and said electric discharging room, said first anode unit and said second anode unit fitting said inner peripheral wall of said housing respectively and spaced from each other;
an insulating fuel layer surrounded by said first anode unit;
a first cathode unit disposed in said triggering room and spaced from said first anode unit, with said insulating fuel layer located between said first anode unit and said first cathode unit;
a main insulating layer surrounded by said first cathode unit; and
a second cathode unit disposed in said housing and inserted from said triggering room into said electric discharging room along said central axis;
wherein said first anode unit, said insulating fuel layer, said first cathode unit, and said main insulating layer are in concentric relationship with one another around said central axis of said housing.
2. The vacuum cathode arc-induced pulsed thruster according to claim 1 , further comprising a control device connected to said first anode unit, said first cathode unit, said second anode unit, and said second cathode unit respectively.
3. The vacuum cathode arc-induced pulsed thruster according to claim 1 , wherein said insulating fuel layer is made of Polytetrafluoroethylene (sold under the trademark TEFLON™).
4. The vacuum cathode arc-induced pulsed thruster according to claim 1 , wherein a partitioning unit projects from said inner peripheral wall of said housing so that said first anode unit and said second anode unit are spaced from each other.
5. The vacuum cathode arc-induced pulsed thruster according to claim 4 , wherein said partitioning unit tapers from said triggering room to said electric discharging room.