Aquila U-8FAILURE LAB / MODEL 0.2

Degraded-system analysis

Compare aggregate system availability and mission effects against the saved Mission 2026-042 baseline.

Open what-if
CONCEPTUAL SIMULATION RESULT

WITHIN CONCEPTUAL CONSTRAINTS

This classification only describes the simplified model constraints below.

PROPULSION AVAILABILITY

8 of 8 motors modeled as available

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POWERED ROTOR AREA19.2 m²
AVAILABLE SHAFT POWER440.0 kW
AVAILABLE STATIC THRUST7,600 N
REQUIRED HOVER THRUST5,886 N
THRUST MARGIN+1,714 N
Estimated range
BASELINE379.5 km
DEGRADED379.5 km
0.0 km
Mission energy
BASELINE15.69 kWh
DEGRADED15.69 kWh
0.00 kWh
End SOC
BASELINE86.9 %
DEGRADED86.9 %
0.0 %
Reserve margin
BASELINE66.9 %
DEGRADED66.9 %
0.0 %
Hover battery power
BASELINE110.4 kW
DEGRADED110.4 kW
0.0 kW
Installed shaft power
BASELINE440.0 kW
DEGRADED440.0 kW
0.0 kW
Thrust margin
BASELINE1,714 N
DEGRADED1,714 N
0 N
Thrust margin
BASELINE29.1 %
DEGRADED29.1 %
0.0 %
WORST UTILIZATION BY CHECK

Constraint comparison

Hover shaft power91.3 / 440.0 kWPASS
Hover battery power110.4 / 400.0 kWPASS
Required hover thrust5,886.0 / 7,600.0 NPASS
Calculated takeoff mass600.0 / 600.0 kgPASS
Required shaft power91.3 / 440.0 kWPASS
Required battery power110.4 / 400.0 kWPASS
Required lift coefficient1.2 / 1.5 ratioPASS
Mission energy15.7 / 96.0 kWhPASS
PHASE ENERGY

Baseline vs degraded

VTOL
1.84 → 1.84 kWh
CLIMB
1.72 → 1.72 kWh
CRUISE
10.18 → 10.18 kWh
DESCENT
0.11 → 0.11 kWh
LAND
1.84 → 1.84 kWh
MODEL BOUNDARY

Limitations and assumptions

  1. Aggregate power and thrust availability only; asymmetric yaw, roll, control allocation, and transient response are not modeled.
  2. A failed motor removes one powered rotor from induced-power area; drag from the inactive rotor is not modeled.
  3. Battery energy retention changes capacity while pack mass remains unchanged.
  4. Battery discharge-power retention is an independent user input; no hidden relationship to energy retention is assumed.
  5. Results are conceptual estimates and are not suitable for safety, certification, or flight-authorization decisions.
BASELINE INPUT HASHfnv1a-a78438c9
DEGRADED INPUT HASHfnv1a-a78438c9