Short S.36
Short S.36 | |
---|---|
Role | Sports aircraft, trainer |
National origin | United Kingdom |
Manufacturer | Short Brothers |
Designer | Horace Short |
First flight | 10 January 1912 |
Number built | 1 |
Variants | Short S.41 Short S.45 |
The Short S.36 was a British two-seat
RNAS and RFC
.
Design and development
The origination of a
E.N.V. Type F, but after Grace's death at the end of the year the project was shelved, the aircraft being completed as a Type S.27.[1] However, when Frank McClean was later shown the design by Horace Short, he asked for one to be built for him, to be powered by a 70 hp (52 kW) Gnome Gamma
engine.
As first built, the aircraft was an unequal-span two-seater
elevator mounted in front of it on top of the fuselage. The centre section of the lower wing was left uncovered, as was the fuselage aft of the cockpit: the cockpit section of the fuselage was covered with plywood, with aluminium panels at the front enclosing the fuel tanks and extending forwards to form the cowling for the front-mounted 70 hp (52 kW) Gnome Lambda engine. The undercarriage consisted of a pair of wheels below the wing leading edge, supplemented by skids extending forward to protect the propeller in case of a nose-over, and a single sprung tailskid mounted under the rear of the fuselage. The fuselage was subsequently rigged lower down, and the aft section of the fuselage covered with fabric.[2]
Service history
The aircraft was first flown by McClean on 10 January 1912,Mortimer Singer Prize for naval officers.
The
Admiralty was sufficiently impressed by the aircraft to order two similar aircraft to be built, these becoming the 100 hp (75 kW) Gnome Double Omega-powered Short S.41 and the 70 hp (52 kW) Gnome Lambda-powered Short S.45
.
Specifications
Data from Barnes 1967, p.87.
General characteristics
- Crew: one
- Capacity: one
- Length: 35 ft 6 in (10.82 m)
- Wingspan: 46 ft 5 in (14.15 m)
- Wing area: 515 sq ft (47.8 m2)
- Empty weight: 850 lb (386 kg)
- Gross weight: 1,300 lb (590 kg)
- Powerplant: 1 × Gnome Gamma 7-cylinder air-cooled rotary piston engine, 70 hp (52 kW)
- Propellers: 2-bladed, 9 ft (2.7 m) diameter
Performance
- Maximum speed: 60 mph (97 km/h, 52 kn)
- Endurance: 6.5 hours
- Wing loading: 3.1 lb/sq ft (15 kg/m2)
References
Wikimedia Commons has media related to Short S.36.