Spitfire Mark I Rotorcraft

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Manufacturer
Spitfire Helicopter Co
Description
The Spitfire Mark I was a utility helicopter built in the United States in the late 1970s and intended for series production.
First Flight
1978-12-01
Designer
Spitfire Helicopter Co
Length (m)
8.96
Height (m)
2.79
Max Speed (km/h)
208
Max Ceiling (m)
4570
Capacity Description
two passengers
National Origin
United States of America
Powerplant Description
1 × Allison 250-C20B, 313 kW (420 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Spitfire_Mark_I
Aircraft Engine
Allison Model 250
Number of Engines
1
Number of main rotor blades
1
50 empty fields

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