As a
solar sail, LightSail's propulsion relies on
solar radiation and not the charged particles of the
solar wind. Solar
photons exert
radiation pressure on the sail, which produces an
acceleration on the spacecraft relative to the ratio of the sail's area to its mass. As such, the design challenge was to maximize the surface area of the sail while minimizing the mass of the spacecraft — all while adhering to the standard 3-unit CubeSat size limitation. LightSail's modular design is based on a modular 3-unit
CubeSat, a small
satellite format created for university-level space projects. One CubeSat-sized module carries the cameras, sensors and control systems, and the other two units contain and deploy the solar sails. The spacecraft contains four triangular sails, which combine to form a rectangular-shaped surface. The sails are made of
Mylar, a reflective
polyester film. LightSail has multiple configurations. It was launched in a stowed configuration with its sails folded within the spacecraft. After launch, it enters an intermediate phase by deploying a small antenna and flipping open its solar panels. This exposes the cameras and reveals the stowed solar sails. To achieve its final "solar sailing" configuration, LightSail extends four 4-meter cobalt alloy booms that slowly spread open the mylar sail material. Using an internal reaction wheel, LightSail 2 is able to orient itself against the
Sun using
Earth's magnetic field as a guide. By "tacking" in and out of the Sun, it can control the force on its sail and thus change its orbit. == Costs and funding ==