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LightSail A, B

LightSail (deployed) [The Planetary Society]

LightSail (before deployment) [The Planetary Society]

LightSail, developed by The Planetary Society, will demonstrate that sunlight alone can propel a spacecraft in Earth orbit. It is a follow up mission to the failed Cosmos 1 project.

Taking advantage of the technological advances in micro- and nano-spacecraft over the past five years, The Planetary Society will build LightSail based on a 3 Unit Cubesat spacecraft. One unit will form the central electronics and control module, and two additional units will house the solar sail module. Cameras, additional sensors, and a control system will be added to the basic Cubesat electronics bus.

LightSail will have four triangular sails, arranged in a diamond shape resembling a giant kite. Constructed of 32 square meters of mylar, LightSail will be placed in an orbit over 800 kilometers above Earth, high enough to escape the drag of Earth’s uppermost atmosphere. At that altitude the spacecraft will be subject only to the force of gravity keeping it in orbit and the pressure of sunlight on its sails increasing the orbital energy. The mission will give a good, clean trial of sunlight as a means of propulsion.

LightSail A was launched in 2015 in a low earth orbit to verify the deployment of the sail, although in this orbit the atmospherical drag prevents solar sailing. LightSail A suffered a software problem after two days, causing the computer to freeze. As it did not respond to reboot commands, it was hoped, that a random radiation induced reboot might solve the problem. The reboot happened after a few days and communications was re-established. The sail was finally deployed on 7 June 2015. Due to the increased drag, the satellite reentered the atmosphere on 15 June 2015 after 25 days on orbit.

LightSail B will be deployed from the Prox 1 microsatellite in a higher orbit and will at first act as a target for proximity operations. After this, it will perform its own solar sailing mission.

Nation: USA
Type / Application: Technology
Operator: The Planetary Society
Contractors: The Planetary Society
Equipment: Solar sail
Configuration: CubeSat (3U)
Propulsion: None
Power: 4 deployable fixed solar arrays, batteries
Lifetime:
Mass: 5 kg
Orbit: 356 km × 700 km, 55.01° (#A)
Satellite COSPAR Date LS Launch Vehicle Remarks
LightSail A 2015-025L 20.05.2015 CC SLC-41 Atlas-5(501) with X-37B OTV-4, GEARRS 2, OptiCube 1, OptiCube 2, OptiCube 3, USS Langley, AeroCube 8A, AeroCube 8B, BRICSat-P, PSat A
LightSail B - 2018 CCK LC-39A Falcon-Heavy with DSX , FORMOSAT 7A, 7B, 7C, 7D, 7E, 7F, GPIM, OTB 1, FalconSat 6, NPSat 1, Oculus-ASR, Prox 1, ARMADILLO, FalconSat 7, TBEx A, TBEx B, Prometheus 2.2, Prometheus 2.4, Prometheus 2.5, Prometheus 2.6, Prometheus 2.7, Prometheus 2.8, Prometheus 2.9, Prometheus 2.10, PSat 2, BRICSat 2, TEPCE 1, TEPCE 2, CP 9 (LEO), StangSat, DOTSI, CNGB, Ballast

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