Hiller ROE Rotorcycle
The Hiller ROE Rotorcycle was a single seat ultralight helicopter designed in 1953 for a military requirement. A total of 12 were produced for the United States Marine Corps. And in 1954, the Hiller Helicopters was selected by the US Navy's Bureau of Aeronautics to build this design of a one man, foldable, self-rescue and observation helicopter. It featured a two blade rotor system. Its original empty weight was 290 lb (132 kg).
primaryTopic
Hiller ROE Rotorcycle
The Hiller ROE Rotorcycle was a single seat ultralight helicopter designed in 1953 for a military requirement. A total of 12 were produced for the United States Marine Corps. And in 1954, the Hiller Helicopters was selected by the US Navy's Bureau of Aeronautics to build this design of a one man, foldable, self-rescue and observation helicopter. It featured a two blade rotor system. Its original empty weight was 290 lb (132 kg).
has abstract
Der Hiller ROE-1 Rotorcycle wa ...... ten flugbereit gemacht werden.
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Hiller ROE Rotorcycle — лёгкий ...... енадцать аппаратов Rotorcycle.
@ru
The Hiller ROE Rotorcycle was ...... ty weight was 290 lb (132 kg).
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manufacturer
number built
origin
Link from a Wikipage to an external page
Wikipage page ID
23,835,284
Wikipage revision ID
714,485,177
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in ground effect
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engine(prop)_
first flight
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228.60000000000002
introduced
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more general
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power original
, later Nelson YO-65-2 four-cylinder, two-cycle engine,
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with pilot and of fuel
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retired
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type of prop
comment
Der Hiller ROE-1 Rotorcycle wa ...... ten flugbereit gemacht werden.
@de
Hiller ROE Rotorcycle — лёгкий ...... енадцать аппаратов Rotorcycle.
@ru
The Hiller ROE Rotorcycle was ...... ty weight was 290 lb (132 kg).
@en
label
Hiller ROE Rotorcycle
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Hiller ROE
@ru
Hiller ROE-1
@de