学术文献库

A technique by which a spacecraft can interact with flows of ionized gas in space (the solar wind or interstellar medium) to be accelerated to velocities greater than the wind velocity is explored. Inspired by the dynamic soaring maneuvers performed by sea birds and gliders in which differences in wind speed are exploited to gain velocity, in the proposed technique a lift-generating spacecraft circles between regions of the heliosphere that have different wind speeds, gaining energy without the use of propellant and only modest onboard power requirements. The spacecraft motion can be modeled as a series of elastic collisions between regions of the medium moving at different speeds. Models of the trajectory are developed to predict the potential velocity gains and the maximum velocity that may be achieved in terms of the lift-to-drag ratio of the vehicle. A lift-generating mechanism is proposed in which power is extracted from the flow over the vehicle in the flight direction and then used to accelerate the surrounding medium in the transverse direction, generating lift. Large values of lift-to-drag ratio are shown to be possible in the case where a small transverse velocity is imparted over a large area of interaction. The requirement for large interaction area in the extremely low density of the heliosphere precludes the use of physical wings, but the use of plasma waves generated by compact, directional antennas to impart momentum on the surrounding medium is feasible, with R-waves, X-waves, Alfven, and magnetosonic waves appearing as promising candidates. A mission is defined in which dynamic soaring is performed on the termination shock of the heliosphere, speeds of 2% of c to be reached within 2.5 years of launch without the expenditure of propellant. The technique may comprise the first stage for a multistage mission to achieve true interstellar flight to other solar systems.