The aircraft was the third iteration of the development of the Servotec Grasshopper, originally designed by Dipl. Ing. J. S. Shapiro

Overview

Data on design, manufacture and status

Design authority: Cierva Rotorcraft Ltd.

Primary manufacturer: Cierva Rotorcraft Ltd.

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Coaxial (x2)

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Width: 9.75 m (32.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: RR Continental O-300 reciprocating

Engine manufacturer: Rolls-Royce Continental

Take-off / rated power: 108 kW (145 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1383 kg (3049 lb)

Max Range: 402 km (217 nm)

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Related Public Resources

Resources related to the CR.LTH-1 Grasshopper III, provided by public sources across the internet.

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