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Model number brantly b-2 b-2b with skid landing gear

General Information of Brantly B-2
Designer : Newby O. Brantly

First Flight : 21 February 1953

Introduction : 1958

Manufacturer : Brantly Helicopter Corporation

Number Built : 334

Role : Light Helicopter

Status : In production (2011)[1]

Unit_Cost : $170,000 in 2003 [2]

General characteristics of Brantly B-2
Crew : 1 (plus 1 pilot)

Disc Area : 442 ft² (41.06 m²)

Empty Weight : 1,020 lb (463 kg)

Height : 6 ft 11 in (2.11 m)

Length : 28 ft (8.41 m[10])

Max Takeoff Weight : 1,670 lb (757 kg)

Powerplant : 1 × Avco Lycoming IVO-360-A1A air-cooled flat-four piston, 180 hp (134 kw)

Rotor Diameter : 23 ft 9 in (7.24 m)

Performance of Brantly B-2
Cruise Speed : 90 mph (78 knots, 145 km/h) (75% power)

Maximum Speed : 100 mph (87 knots, 161 km/h) at sea level

Range : 250 miles (217 NM, 400 km)

Rate Of Climb : 1,900 ft/min (9.7 m/s)

Service Ceiling : 10,800 ft (3290 m)

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