The Holmes KH-1 is a British single-seat high-performance homebuilt sailplane designed and built by Kenneth Holmes and first flown on 27 November 1971.
Design The KH-1 is a shoulder-wing cantilever monoplane with a conventional all-wood semi-monocoque fuselage and tail unit with an all-moving tailplane, the wings have small-span flaps for control during approach but no airbrakes or spoilers. The pilot has a semi-reclined seat in an enclosed cockpit under a two-piece transparent canopy. The KH-1 landing gear is a retractable monowheel gear and a tailskid, it is also fitted with a tail drag chute to control speed during approach.
Specifications Data from Jane's All the World's Aircraft 1973-74General characteristics Crew: 1 Length: 7.315 m (24 ft 0 in) Wingspan: 18.56 m (61 ft 0 in) Wing area: 11.70 m2 (126 sq ft) Empty weight: 226 kg (500 lb) Gross weight: 325 kg (716 lb) Performance
Maximum speed: 158 km/h (97.5 mph, 84.7 kn) Stall speed: 67 km/h (41.5 mph, 36.1 kn)
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External links Image of Holmes KH-1 in 1971
