They proposed a
free return trajectory to allow the
spacecraft to use the smallest possible amount of
propellant to flyby Mars and return to Earth. They stated that the January 2018 launch window offered a rare orbit opportunity to travel to Mars and return to Earth in 501 days. Their stated backup plan involved a mission beginning in 2021 but it would be 88 days longer. They stated it would require both a flyby of Venus and Mars. The flight would take the spacecraft within 800 kilometres of the surface of Venus, using the planet for a
gravity assist to speed the travel to Mars. According to a paper written by Tito, "the mission would require no maneuvers except small course corrections after a
trans-Martian injection burn, [and] would allow no aborts. ... [It will] use
low Earth orbit launch and
crewed-spacecraft technology, outfitted for the long duration of a flight to Mars." They speculated that when the spacecraft returned to Earth it would reenter the atmosphere at 50 000 km per hour (ca 13.9 km/s), faster than any previous return.
Student design competition During the 16th Annual International Mars Society Convention in 2013, the Mars Society announced an international engineering competition for student teams to propose designs for the architecture of the mission. The contest was open to university engineering student teams. The design contest took place on 9 August 2014, and was won by an international team from
Purdue University in US and
Keio University in Japan. ==Criticism==