Solar sail might enable 'Polar-sitting' orbit
26 February 2016
The VisionSpace project suggests there may be alternatives to conventional elliptical ‘Keplerian’ orbits such as this 'hovering' orbit assisted by solar sails.
This image (courtesy of ESA/Hubble/Jeannette Heiligers) shows how a large solar sail-equipped satellite could partly offset Earth’s and the Sun’s gravity with the slight but steady pressure of sunlight to hover above the Arctic or Antarctic, enabling continuous coverage of high-latitude regions for climate observation or regional communication services.
“Standard space missions employ conventional elliptical ‘Keplerian’ orbits,” says Colin McInnes, Professor of Engineering Science at the UK’s University of Glasgow. “However, our VisionSpace project has been investigating novel families of orbits and space systems across a broad range of sizes that could make use of additional factors such as solar radiation pressure, air drag or gravitational interactions.
“The space systems range from microscale applications such as satellite swarms and dust clouds, to mesoscale large deployable space webs and solar sails, all the way up to macroscale solutions such as asteroid capture.”
was a five-year project ending in 2014 to research space system engineering across the extremes of size, funded by the European Research Council.
Professor McInnes, who oversaw the project while at the University of Strathclyde, was recently invited to ESA’s ESTEC technical centre by the Agency’s Advanced Concepts Team (ACT) to highlight the project’s findings. The ACT is tasked with peering beyond the horizon of current space projects.