Hall effect thruster and a space vehicle including such a thruster
US-10131453-B2 · Nov 20, 2018 · US
US2019010933A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2019010933-A1 |
| Application number | US-201716066899-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 6, 2017 |
| Priority date | Jan 8, 2016 |
| Publication date | Jan 10, 2019 |
| Grant date | — |
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A plasma accelerating apparatus includes: a cathode ( 11 ) configured to supply electrons to a plasma acceleration region; a anode ( 12 ); a power supply ( 13 ) configured to apply a voltage between the cathode and the anode; a supply port ( 14 ) arranged on an outer circumference side than the cathode to supply a propellant to the plasma acceleration region; and a first magnetic field generator ( 15 ) configured to generate a first axial direction magnetic field in the upstream side region of the plasma acceleration region to suppress that the electrons supplied from the cathode head for the anode. Thus, the plasma accelerating apparatus and the plasma accelerating method having high thrust efficiency can be provided.
Opening claim text (preview).
1 - 12 . (canceled) 13 . A plasma accelerating apparatus comprising: a cathode configured to emit electrons to a direction of a predetermined center axis to supply the electrons to an upstream side region of a plasma acceleration region; an anode having a ring shape when viewing from the direction of the center axis and arranged around the center axis; a power supply configured to apply a voltage between the cathode and the anode; a supply port arranged on an outer circumference side than the cathode to supply a propellant before plasmatization or a propellant after plasmatization to the plasma acceleration region; and a first magnetic field generator arranged in a second direction from the plasma acceleration region when a motion direction of the electrons emitted from the cathode is defined as a first direction and a direction opposite to the first direction is defined as the second direction, and configured to generate a first axial direction magnetic field in the upstream side region of the plasma acceleration region to suppress that the electrons supplied from the cathode head for the anode, wherein the first axial direction magnetic field has an axial direction component which is a component parallel to the center axis and monotonously degreases as heading for the first direction from the second direction on the center axis in the upstream side region of the plasma acceleration region, and a radial direction component which is a component orthogonal to the center axis and monotonously increases as heading for the first direction from the second direction on the center axis in the upstream side region of the plasma acceleration region, and wherein the first magnetic field generator is arranged in the second direction from the supply port. 14 . The plasma accelerating apparatus according to claim 13 , wherein the first magnetic field generator is arranged in the second direction from an end of the plasma acceleration region in the second direction. 15 . The plasma accelerating apparatus according to claim 13 , wherein the first magnetic field generator is arranged on the outer circumference side than the cathode, and wherein the supply port is arranged on the outer circumference side than the first magnetic field generator. 16 . The plasma accelerating apparatus according to claim 13 , wherein the supply port is arranged on the outer circumference side than the cathode, and wherein the first magnetic field generator is arranged on the outer circumference side than the supply port. 17 . The plasma accelerating apparatus according to claim 13 , further comprising: an orientation changing mechanism configured to change an orientation of the first magnetic field generator. 18 . The plasma accelerating apparatus according to claim 13 , further comprising: a second magnetic field generator configured to generate a second axial direction magnetic field in the plasma acceleration region, wherein a direction of the second axial direction magnetic field generated by the second magnetic field generator is different from the direction of the first axial direction magnetic field generated by the first magnetic field generator. 19 . The plasma accelerating apparatus according to claim 13 , further comprising: a first wall section in contact with the plasma acceleration region; an electron emission port arranged in the first wall section to emit the electrons supplied from the cathode. 20 . The plasma accelerating apparatus according to claim 19 , wherein the anode is arranged on the first wall section. 21 . The plasma accelerating apparatus according to claim 13 , wherein the anode is arranged on the outer circumference side than the supply port. 22 . The plasma accelerating apparatus according to claim 13 , further comprising: a first wall section in contact with the plasma acceleration region, wherein the anode has a ring shape, and wherein a distance between the first wall section and a downstream side end surface of the anode is equal to or less than ⅓ of the inner diameter of the anode. 23 . A plasma accelerating method using a plasma accelerating apparatus, wherein the plasma accelerating apparatus comprises: a cathode configured to emit electrons to a direction of a predetermined center axis to supply electrons to a plasma acceleration region; an anode having a ring shape when viewing from the direction of the center axis and arranged around the center axis; and a magnetic field generator arranged in a second direction from the plasma acceleration region, when a first direction is defined as a direction of movement of the electrons emitted from the cathode, and the second direction is defined as a direction opposite to the first direction, the plasma accelerating method comprising: generating a fan-shaped magnetic field in the plasma acceleration region by using the magnetic field generator; applying a voltage between the cathode and the anode; carrying out a first supply of supplying the electrons supplied from the cathode into the fan-shaped magnetic field; carrying out a second supply of supplying a propellant before plasmatization or a propellant after plasmatization into the plasma acceleration region for the first direction from a supply port; accelerating ions in a plasma generated in the plasma acceleration region by using an electric field generated by the anode and the electrons in the fan-shaped magnetic field so as to be focused for the center axis; and neutralizing the ions through collision of the ions and the electrons in the fan-shaped magnetic field, wherein the fan-shaped magnetic field has an axial direction component which is a component parallel to the center axis and monotonously degreases as heading for the first direction from the second direction on the center axis in the upstream side region of the plasma acceleration region, and a radial direction component which is a component orthogonal to the center axis and monotonously increases as heading for the first direction from the second direction on the center axis in the upstream side region of the plasma acceleration region, and wherein the magnetic field generator is arranged in the second direction from the supply port. 24 . The plasma accelerating method according to claim 23 , further comprising: generating a Hall current through interaction of a fan-shaped magnetic field and an electric field generated between the cathode and the anode; and generating a plasma in the plasma acceleration region through collision of a propellant before plasmatization or a propellant after plasmatization supplied into the plasma acceleration region and the electrons of the Hall current.
with a central channel, e.g. end-Hall type · CPC title
Plasma accelerators · CPC title
using magnetic fields substantially generated by the discharge in the plasma · CPC title
Means for supplying the propellant · CPC title
grid-less with an applied magnetic field · CPC title
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