# Thrust vectoring of an electric solar wind sail with a realistic sail shape

## TL;DR

This paper models the shape of a rotating electric solar wind sail under realistic conditions, deriving equations for its shape and analyzing how it affects thrust vectoring and attitude control.

## Contribution

It introduces a new analytical approximation for the sail shape considering centrifugal and solar wind forces, improving understanding of sail attitude maintenance.

## Key findings

- The sail shape transitions from conical near the spacecraft to flattened at the rim.
- The required voltage modulation for attitude control is smaller than previous rigid tether models.
- Thrust vectoring can be effectively achieved with reduced thrusting margin.

## Abstract

The shape of a rotating electric solar wind sail under the centrifugal force and solar wind dynamic pressure is modeled to address the sail attitude maintenance and thrust vectoring. The sail rig assumes centrifugally stretched main tethers that extend radially outward from the spacecraft in the sail spin plane. Furthermore, the tips of the main tethers host remote units that are connected by auxiliary tethers at the sail rim. Here, we derive the equation of main tether shape and present both a numerical solution and an analytical approximation for the shape as parametrized both by the ratio of the electric sail force to the centrifugal force and the sail orientation with respect to the solar wind direction. The resulting shape is such that near the spacecraft, the roots of the main tethers form a cone, whereas towards the rim, this coning is flattened by the centrifugal force, and the sail is coplanar with the sail spin plane. Our approximation for the sail shape is parametrized only by the tether root coning angle and the main tether length. Using the approximate shape, we obtain the torque and thrust of the electric sail force applied to the sail. As a result, the amplitude of the tether voltage modulation required for the maintenance of the sail attitude is given as a torque-free solution. The amplitude is smaller than that previously obtained for a rigid single tether resembling a spherical pendulum. This implies that less thrusting margin is required for the maintenance of the sail attitude. For a given voltage modulation, the thrust vectoring is then considered in terms of the radial and transverse thrust components.