ASJA Viking I

The Viking I was a utility aircraft designed in Sweden for the Swedish Air Force

2 prototypes were built with no interest shown.

The 2 prototypes were sold to private buyers.

Variants

The 1^st built aircraft originally mounted the British Cirrus Hermes IIB engine.

The second built aircraft was built with the Walter Mars engine.

Specifications

Crew

1 pilot

Capacity

2 passengers

Range

11.2 m

Length

8.0 and 8.2 m

Height

2.4 and 3.0 m

Supporting surface

22.0 m2

Surface load

48.4 and 51.1 kg/m2

Empty aircraft weight

665 and 775 kg

Take-off weight

1 065 and 1 125 kg

Powerplants

110 kW Cirrus Hermes IIB, inline air cooled four cylinder engine

Walter Mars 145/150 k, (106.6/110.3 kW) air cooled nine cylinder engine

Walter Gemma 150/165 k, (110.3/121.3 kW) air cooled nine cylinder engine

Propeller

Solid metal propeller

Performance

Top speed

170 and 165 km/h, with Gemma engine: 210 km/h

Cruising speed

155 and 150 km/h, with Gemma engine 185 km/h

Landing speed

70 and 75 km/h

Practical access

4,200 and 3000 m

Access up

Up to 1000 m 6.5 min.

Range

620 and 600 km.