DOES NOT CLOSE: DivergedLimit: 23.5 kg (25kg - 1.5kg margin)
Evaluating configuration...
Converged MTOW
N/Akg
Frame Law: N/A kg
Outbound / Total Range
35.0km
Total: 70.0 km
Cruise Airspeed
N/Am/s
L/D: N/A
Buffer Battery
N/Akg
By: N/A
H2 Fuel Required
N/Ag
None selected
Payload vs. Range Envelope Curve
Sub-25kg MTOW constraint envelope under 45.0 °C ambient air density (live solver)
Envelope Curve Current Operating Point
Real Aircraft Mass Breakdown (Group Resizing)
Mass scaled via real structural laws from configure.py groups
Total MTOW
18.09 kg
Ceiling≤ 23.5 kg5.41 kg margin
Wing Aerodynamic Surface2.10kg (11.6%)
Fuselage & Skid Gear3.06kg (16.9%)
Booms & Inverted-V Tail1.93kg (10.7%)
VTOL Lift Drive Units & Props2.50kg (13.8%)
Cruise Pusher & Drive0.49kg (2.7%)
Fuel Cell & TMS Ducting2.00kg (11.1%)
H2 Cylinder & Gas Mass0.00kg (0.0%)
Buffer Battery Pack1.00kg (5.5%)
BVLOS Avionics & Satcom2.00kg (11.1%)
Parachute (SAF) & Harness2.01kg (11.1%)
Delivered Payload1.00kg (5.5%)