The VTOL Aircraft Phillicopter is a 1970s Australian light utility helicopter designed and built by VTOL Aircraft of Newcastle West, New South Wales.[1]
Phillicopter | |
---|---|
Role | Light utility helicopter |
National origin | Australia |
Manufacturer | VTOL Aircraft |
First flight | 1971 |
Duan A. Phillips began work on design of a two-seat helicopter in 1962, and started to build a prototype in 1967. The prototype, the Phillicopter Mark I, was completed and first flew in 1971, powered by a single 145 hp (108 kW) Rolls-Royce Continental O-200 engine.[2] Phillips set up VTOL Aircraft Pty Ltd in 1971 to construct and develop the Phillicopter.[3] The Phillicopter was granted its Australian type certificate in 1984,[4] and the prototype was modified to represent a pre-production standard.[5]
The Phillicopter is a conventional two-seat helicopter with a two-blade rotor powered by a 180 hp (134 kW) Lycoming O-360 piston engine.[1] It has an enclosed cabin with removable doors and is fitted with dual controls.[1] The open frame fuselage has a two-blade tail rotor at the rear.[1] A 91-litre fuel tank is fitted and an optional 91-litre central tank can be fitted, although this can also be used for crop spraying chemicals rather than fuel.[1] The Phillicopter has a fixed skid type landing gear.[1]
Data from [1]Brassey's World Aircraft & Systems Directory
General characteristics
Performance
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