Orrery

ORRERY DEMO PRE-LAUNCH

This is a placeholder free-return demo. Pick a real mission to see its actual launch window.

TRAJECTORY Heliocentric free-return

VEHICLE Falcon Heavy

DEPARTURE Earth dep

ARRIVAL Earth return

MET DAY 0

HELIO ∆V 32.73 km/s

FROM EARTH 0.00 M km · 0.00 l-min

FROM MARS 149 M km

∆V USED 3.61 km/s

∆V REMAINING 0.25 km/s

ETA DAY 509

CRITICAL ∆v margin 0.25 km/s

ONE-WAY 0.00 l-min

ROUND TRIP 0.00 l-min