Hover endurance is usable energy over hover power
Each rotor carries T/n of the weight. Actuator-disk theory gives an induced velocity vi = √(Ti / (2 ρ A)) and an ideal hover power Pideal = n Ti vi = T √(T / (2 ρ n A)). The shaft (or electrical, at the motors) power is that ideal power divided by a figure of merit FM, plus any avionics load you enter. Endurance is usable battery watt-hours times 3,600, divided by that power. A 2 kg quad on four 0.25 m rotors, FM = 0.60, and 80 Wh usable typically hovers for on the order of tens of minutes at a few hundred watts — a sanity check, not a sales-sheet number.
Forward flight, a climbing profile, wind, battery sag, and motor or ESC efficiency away from the hover point all change the real time. If you care about rotor disk power or a hover ceiling rather than a battery, see the hover power calculator; for a larger electric airplane, see electric aircraft endurance.
Sources
- Momentum / actuator-disk theory (Gessow and Myers; Leishman, Principles of Helicopter Aerodynamics).
- Hover figure of merit, FM = Pideal / Pactual.
- Electric energy endurance t = E / P.
Frequently asked questions
Why is hover time shorter than the time printed on the box?
Manufacturer ratings often include a lighter aircraft, a partial throttle cruise, or a larger usable fraction than 80%. This page is a hover, at the weight you type.
What figure of merit should I use?
Small consumer quads often sit around 0.5–0.7. A 0.60 default is a middle value, not a measurement of your props.
Does this include reserve or a landing battery margin?
Only through the usable fraction. Tighten it if you want a reserve built in.