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/ ASJA Viking I
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.
built aircraft originally mounted the British Cirrus Hermes IIB engine.
The second built aircraft was built with the Walter Mars engine.
8.0 and 8.2 m
2.4 and 3.0 m
48.4 and 51.1 kg/m2
Empty aircraft weight
665 and 775 kg
1 065 and 1 125 kg
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
Solid metal propeller
170 and 165 km/h, with Gemma engine: 210 km/h
155 and 150 km/h, with Gemma engine 185 km/h
70 and 75 km/h
4,200 and 3000 m
Up to 1000 m 6.5 min.
620 and 600 km.
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