Small, single-seat autogyro From Wikipedia, the free encyclopedia
The Bensen B-8 is a small, single-seat autogyro developed in the United States in the 1950s. Although the original manufacturer stopped production in 1987, plans for homebuilders are still available as of 2019.[needs update] Its design was a refinement of the Bensen B-7, and like that aircraft, the B-8 was initially built as an unpowered rotor-kite. It first flew in this form in 1955, and on 6 December a powered version, designated B-8M (M for motorised) first flew. The design proved to be extremely popular and long-lasting, with thousands of sets of plans sold over the next thirty years.
The B-8's design is extremely minimalist, with not much more to the aircraft than a pilot's seat, a single tailfin, a rotor, and (in powered versions) the powerplant. In May 1968 a B-8 and B-8M were studied by the USAF under the Discretionary Descent Vehicle (DDV) program as the X-25B and X-25A respectively. In this scheme, it was proposed to integrate combat aircraft ejection seats with a small autogyro or rotor kite to allow downed pilots more control over their post-ejection landing spot. The X-25A and X-25B were used to evaluate the piloting and training requirements of the autogyros. No full-scale operational tests were ever performed. The U.S. Air Force stopped funding the DDV program with the end of the Vietnam War.[2]
One B-8M, named Spirit of Kitty Hawk (registration N2588B) was used to make a special commemorative flight exactly duplicating the first flight of the Wright brothers' original Flyer on the sixtieth anniversary of the occasion. This same aircraft was flown by Igor Bensen himself between May 1967 and June 1968 to set twelve world and US speed, distance, and altitude records for autogyros, the largest number of such records to be held by any non-military rotorcraft.[citation needed]
B-8 Gyro-Glider - unpowered rotor-kite intended to be towed behind a car
B-8B Hydro-Boat - B-8 with a full boat hull intended to be towed behind another boat
B-8M Gyro-Copter - standard motorised version, main production type. Usually powered by a McCulloch 4318 engine
B-8MH Hover-Gyro - twin, coaxial rotor design with powered lower rotor and autorotating upper rotor, giving it the capability of hovering. Upper rotor and drive propeller powered by separate engines
B-8MJ Gyro-Copter - B-8M modified for "jump" take off by a small second engine providing power to rotor head with anti-torque provided by rudder correction under power.[3]X-25A 68-10770 in flight
B-8W Hydro-Glider - float-equipped B-8 intended to be towed behind a boat[4]
X-25B - B-8 evaluated by USAF. Single example (serial 68-10771) first flown 23 January 1968 and preserved at the AFFTC Museum at Edwards Air Force Base.
Rotorcraft Minicopter Mk 1 - South African variant with pre-rotator and cockpit fairing.[5]
Aeroflyte DGH-1 - 70hp (52kW) license-built model from Aeroflyte.[6]
Data from Jane's All The World's Aircraft 1982–83[10]
General characteristics
Crew: 1
Length: 11ft 4in (3.45m)
Height: 6ft 3in (1.91m)
Empty weight: 247lb (112kg)
Max takeoff weight: 500lb (227kg)
Fuel capacity: 6USgal (5.0impgal; 22.7L) or 9.7USgal (8.1impgal; 36.7L) in a combined seat/fuel tank, with provision for an auxiliary tank for ferrying