Electric power
Previous Venus landers have relied on batteries for electric power, which limits operation to a few hours at most, relying on thermal mass to delay the death of the system due to overheating. The power system for this mission uses sodium–sulfur batteries (NaS) that are re-charged by solar arrays and can function under Venus surface conditions without the need for heavy cooling systems.Landis, G. A. and Harrison, R. (2008) "Batteries for Venus Surface Operation," ''Journal of Propulsion and Power'', Vol. 26, Number 4, 649-654, July/Aug 2010; originally presented as paper AIAA-2008-5796, 6th AIAA International Energy Conversion Engineering Conf., Cleveland OH, July 28–30, 2008. The wingsail and upper deck would be covered with solar panels made ofWind force
While the wind speed at the surface of Venus is , at Venus pressure and density (65 kg/m3), even low wind speeds develop significant force.Wingsail
Science payload
Orbiter
Because of the thick Venus atmosphere, radio signals from the rover would lack the power and reach, so a relay orbiter needs to be incorporated in the mission architecture. After ''Zephyr'' separation, the orbiter would propulsively brake into a highly eccentric orbit around the planet. This orbit would have a 24 hr period, permitting communication with ''Zephyr'' for 12 to 18 hr during each orbit. When Venus is at its closest to Earth, the communications time-lag from Venus and Earth is approximately four minutes, which is too long to control from Earth in real time, so the rover would be parked most of the time performing observations with the sail slack, while the ground controllers examine the terrain and decide the next target. If selected for funding, the relay orbiter could also host some science instruments.References
{{Venus spacecraft Missions to Venus Proposed NASA space probes Three-wheeled robots Wind-powered vehicles