Mission Assessment
Mission Assessment
Size propulsion and maneuvers for a mission: build the plan, get a complete explainable Δv budget, recalculated live as you edit.
01
Spacecraft
Dry mass
150 kg
Wet mass
165.0 kg
Propulsion
Propellant is sized sequentially per line with the Tsiolkovsky rocket equation at this specific impulse — each line burns from the mass the previous line left.
Drag environment
Drag area and drag coefficient feed the SMA-maintenance atmospheric-drag computation.
