Alpha 800 Airframe. Technical specifications

Power Plant

Two stroke gasoline engine
Displacement 32 cc
Maximum output 2.4 kW
Maximum torque

2.0 N-m

Dimensions

Length1.7 m
Height0.6 m
Rotor diameter

1.8 m

Performance

Cruise speed55 km/h
Endurance 2.5 hrs*
Ceiling

3.000 m

Weight

Max. take-off weight14 Kg
Max. payload3 Kg

Launch & Recovery

Vertical take-off & landing (VTOL)

Payloads

EO/IR, gyrostabilized, geo-referenced
LIDAR, infrared or multispectral
Radio relay, Laser Altimeter, Transponder

Structure Material

Carbon fiber

Complete System Transport Case

Dimensions1.80 m x 0.7 m x 0.9 m
Optional weatherized/ruggedized

*Typical endurance with 12.5 Kg of TOW (1.5 KG payload), ISA and sea-level
 Maximum endurance at cruise speed 2 hours 50 minutes.
 Maximum endurance 100% hover: 2 hours.
 Typical endurance (50% cruise  speed, 50% hover): 2 hours 30 minutes.

Payload bays (PB)

Number of configurations 2
Configuration 1 – PB 1, 3, 4, 5
Configuration 2 – PB 2, 3, 4, 5

Payload bay 1 – Main sensor

Dimensions:

Typical weight: 1Kg

Payload bay 2 – Belly sensor

Dimensions:

Typical weight: 1.8Kg

Payload bay 3 – PCM bay

Dimensions:

Typical weight: 400 gr.

Payload bay 4 – Power board bay

Dimensions:

Typical weight: 300 gr.

Payload bay 5 – Autopilot bay

Typical weight: 180 gr.

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