Trisha Shetty (Editor)

Holmes KH 1

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Top speed
  
158 km/h

Length
  
7.32 m

Wingspan
  
19 m

First flight
  
November 27, 1971

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.

Contents

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 1973-74

General 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 ft2)
  • Empty weight: 226 kg (500 lb)
  • Gross weight: 325 kg (716 lb)
  • Performance

  • Maximum speed: 158 km/h (97.5 mph)
  • Stall speed: 67 km/h (41.5 mph)
  • References

    Holmes KH-1 Wikipedia