Descripción del producto
The Robinson R*2 is a two-bladed, single-engine light utility
helicopter manufactured by Robinson Helicopter Company. The
two-seat R*2 was designed in ***3 by Frank Robinson and has been
in production since ***9.
General characteristics
Crew: 1
Capacity: 2, including pilot
Length: *8 ft 8 in (8.*4 m)
Rotor diameter: *5 ft 2.4 in (7.*7 m)
Tail rotor diameter: 3 ft 6 in (1.*7 m)
Height: 8 ft *1 in (2.*2 m)
Disc area: **7 ft² (*6.2 m²)
Empty weight: **0 lb (**9 kg[*3])
Loaded weight: **0 lb (**7 kg)
Max. takeoff weight: 1,**0 lb (**5 kg)
Main tank total capacity: *9.8 US gallons (*5 liters)
Main tank usable capacity: *9.2 US gallons (*3 liters)
Optional aux tank total capacity: *0.9 US gallons (*1 liters)
Optional aux tank usable capacity: *0.5 US gallons (*0 liters)
Powerplant: 1 × Lycoming O****-A2B or -A2C flat 4 piston engine,
**4 hp (*3 kW)
Performance
Never exceed speed: **7 mph, **8 km/h, **2 kts
Cruise speed: **0 mph, **7 km/h, *6 kts
Range: **0 mi (**6 km)
Service ceiling: *4,**0 ft (4,**7 m)
Rate of climb: 1,**0 ft/min (6.1 m/s)
Disc loading: 2.*1 lb/ft² (*3.7 kg/m²)
Fuel consumption: 8~*0 US Gal/hr
Power/mass: 0.**5 hp/lb (0.**7 kW/kg)
Endurance: approx. 3 hours, with **-minute reserve
Role Robinson,Light utility and trainerhelicopter,turbofan
Manufacturer Robinson Helicopter Company
Designer Frank D. Robinson
First flight ***5
Introduction ***9
Status in production (*2 in ***4)[1]
Number built over 4,**0 (***5)
Unit cost $**8,**0 (as of August ***6)
Developed into Robinson R*4
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