Using: OAT
+15°C, SOH
95%, Alt
1,525 ft — set in
Route Planner
· ISA temp:
— · ISA deviation:
—
Aircraft reference speeds
Rate of climb — Vy = 75 KIAS · 600 kg
Pressure
Altitude (ft) | Rate of Climb [ft/min] |
|---|
| ISA −15°C | ISA −5°C | ISA | ISA +5°C | ISA +15°C |
|---|
Interpolated ROC at current altitude & OAT
Cruise power setting
Selected: —
%SOC per flight phase
Interpolated for SOH = 80%. Source: POH energy management tables.
| Flight phase | At SOH | Battery State of Health (%SOH) |
|---|
| 100 | 80 | 60 | 40 | 20 | 0 |
|---|
Computed performance — used by route planner
Settings are saved automatically to your browser and applied when you open the
Route Planner.
Data source — Pipistrel Velis Electro POH
Rate of climb: 600 kg MTOM, Vy = 75 KIAS, full power 48 kW.
%SOC table: energy management section, SOH-dependent.
Cruise power: level flight at MTOM.
Glide: Vglide = 70 KIAS, ratio 15:1, 0 kW (power off).