Lockspeiser LDA-01
| Land Development Aircraft | |
|---|---|
 | |
| Role | Experimental utility transport |
| Manufacturer | Lockspeiser |
| Designer | David Lockspeiser |
| First flight | 24 August 1971 |
| Status | Destroyed, cancelled from register. |
| Number built | 1 |
|
| |
The Lockspeiser LDA-01 ("Land Development Aircraft") was a British seven-tenths scale research and development tandem wing aircraft,[1] which was designed and built by the late David Lockspeiser to prove a concept for a low-cost utility transport.
Design and development
The LDA-01 was a single-seat tandem-wing monoplane, fabric covered with metal construction. The foreplane had a common design to the separately-made port and starboard wings of the main plane, giving it half the area. The intention was to reduce the number of spare parts needed by re-using the same wing component interchangeably in each location.[2] The main wings were mounted at the rear-end of the box structure fuselage and the fore wing was attached underneath the front. The fuselage was fitted with a four wheeled landing gear and was designed to be fitted with a detachable payload container to allow easy conversion between roles. It was powered by a rear-mounted pusher engine. The LDA-01 G-AVOR first flew on 24 August 1971 at Wisley in Surrey, under the power of an 85 hp (63 kW) Continental C85 piston engine, but was later refitted with a more powerful Lycoming O-320 engine.
The aircraft (which by this time had been re-registered G-UTIL), and had been renamed the Boxer 500, was being modified to planned production configuration by Brooklands Aerospace at Old Sarum Airfield when it was destroyed in a fire on 16 January 1987.[3][4][5]
Specifications
Data from British Civil Aircraft since 1919 and Jane's All The World's Aircraft 1976-77.[6][7]
General characteristics
- Crew: One
- Length: 22 ft 6 in (6.86 m)
- Wingspan: 29 ft 0 in (8.84 m)
- Height: 9 ft 1 in (2.77 m)
- Wing area: 112.6 ft2 (10.46 m2)
- Empty weight: 1,236 lb (561 kg)
- Gross weight: 1,617 lb (733 kg)
- Powerplant: 1 × Lycoming O-320, 160 hp (119 kW)
Performance
- Cruise speed: 106 mph (170 km/h)
- Range: 299 miles (481 km)
References
- ↑ "Flight International report" (pdf), Flight International: 673, 24 April 1975
- ↑ Lockspeiser, D,; "Aerial Land Rover", Flight, 9 September 1971, pages 404-405.
- ↑ "GINFO Search Results, G-AVOR". CAA. Retrieved 2008-01-07.
- ↑ "GINFO Search Results, G-UTIL". CAA. Retrieved 2008-01-07.
- ↑ Walters Air International August 1991, pp. 71–72.
- ↑ Jackson 1974, p.259
- ↑ Taylor 1976, p.190
- Jackson, A.J. British Civil Aircraft since 1919 Volume 3, 1974, Putnam, London, ISBN 0-370-10014-X, Page 259
- Taylor, John W.R, (ed). Jane's All The World's Aircraft 1976-77. London: Macdonald and Jane's. 1976. Page 190. ISBN 0-354-00538-3.
- Walters, Brian. "LDA - Phoenix or dead duck?" Air International. Vol. 41 No. 2. August 1991. pp. 71–72. ISSN 0306-5634.
External links
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Wikimedia Commons has media related to Lockspeiser LDA-1. |