Electric sail with voltage multipliers in tethers
The effective area of an electric sail depends on the voltage applied to tethers. The use of higher voltages is made possible by moving voltage multipliers to tethers, perhaps 100 meters out from the body of the spacecraft.
1. A tether for use in an electric sail powered spacecraft, comprising:
a low-voltage tether electrically connected to a low-voltage end of a voltage multiplier and an output of a control voltage generator;
a high-voltage tether, whose length is at least one kilometer, electrically connected to the high-voltage end of the voltage multiplier; and
a load-bearing insulating member carrying load from the high voltage tether to the support structure of the spacecraft,
wherein the voltage multiplier can be deployed outside the spacecraft at a sufficient isolation distance from other parts of the spacecraft and wherein the load-bearing insulating member carries the load to the support structure via the low-voltage tether.
2. The tether of claim 1 , wherein the voltage multiplier is located inside the load-bearing insulating member.
3. The tether of claim 1 , further comprising a reel attached to the load-bearing insulating member for deploying the high-voltage tether by unwinding it from the reel.
4. A method of generating a high voltage for a tether in an electric sail powered spacecraft, comprising:
generating a control voltage;
driving a voltage multiplier located outside the spacecraft at a sufficient isolation distance from other parts of the spacecraft from the control voltage via a low-voltage tether;
driving one or more high-voltage tethers from an output of the voltage multiplier, the one or more high-voltage tethers being at least one kilometer long; and
using a load-bearing insulating member to carry load from the high-voltage tether to a support structure of the spacecraft,
wherein the load is carried from the high-voltage tether to the support structure via the low-voltage tether.
5. An electric sail powered spacecraft comprising:
a plurality of tethers, at least one tether comprising a load-bearing insulating member, a low-voltage tether, and a high voltage tether, with the length of the high-voltage tether being at least one kilometer; and
a control voltage generator electrically connected via the low-voltage tether to the low-voltage end of a voltage multiplier whose high-voltage end is electrically connected to the high-voltage tether,
wherein the voltage multiplier can be deployed outside the spacecraft at a sufficient isolation distance from other parts of the spacecraft and wherein load is carried from the high voltage tether to the support structure via the low-voltage tether.