The Praga E-40 was a single engine, two seat, biplane basic trainer, built in Czechoslovakia in the mid-1930s.
| Praga E-40 | |
|---|---|
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| |
| Role | Basic trainer |
| National origin | Czechoslovakia |
| Manufacturer | ČKD-Praga |
| First flight | c.1936 |
| Number built | 1? |
Design and development edit
The E-40, one of several Praga trainer designs, was a single-bay biplane with open, tandem cockpits. The swept wings had twin wooden spars and a mixture of plywood and fabric covering. Ailerons were fitted to the lower wing and the upper wing had a cut-out on its trailing edge to enhance visibility from the forward cockpit. The N-form interplane struts were steel and the bay braced with streamlined wires. A pair of vertical N-form struts joined the wing centre section to the upper fuselage. The fixed tail surfaces were wood framed and plywood covered; the tailplane was strut braced from below. Elevators and rudder were fabric covered over steel frames. The rudder had a trim tab.[1]
The fuselage of the E-40 was a steel structure, rigidly braced at the front and wire braced aft. The nose and the upper decking were covered with detachable steel panels; fabric covering was used elsewhere. Fuel and engine oil tanks were in the fuselage. The E-40 was powered by a four-cylinder 63/71 kW (85/95 hp) Walter Minor air-cooled, inverted piston engine driving a two-blade propeller. It had a split type main undercarriage with wheels on V-form legs mounted just forward of the wing leading edge. Rubber-in-compression spring units were mounted in extended hubs; the pistons of these units were held in place on a shallow, inverted V strut, itself attached to the lower fuselage via a steel tube pyramid. The tailwheel castored and had rubber springing within the rear fuselage.[1]
Operational history edit
There are no records of the E-40 entering production and it is possible that only the prototype, OK-EDA,[2][3] was built.
Specifications edit
Data from Jane's All the World's Aircraft 1938.[1]
General characteristics
- Crew: 2
- Length: 8.15 m (26 ft 9 in)
- Wingspan: 9.0 m (29 ft 6 in)
- Height: 2.85 m (9 ft 4 in)
- Wing area: 20.6 m2 (222 sq ft)
- Empty weight: 470 kg (1,036 lb)
- Gross weight: 720 kg (1,587 lb)
- Powerplant: 1 × Walter Minor 4-cylinder inverted air-cooled, 63 kW (85 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 165 km/h (103 mph, 89 kn)
- Cruise speed: 135 km/h (84 mph, 73 kn)
- Range: 500 km (310 mi, 270 nmi)
- Service ceiling: 4,000 m (13,000 ft)
- Time to altitude: 16 min to 2,000 m (6,560 ft)
References edit
- ^ a b c Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. p. 95c. ISBN 0-7153-5734-4.
- ^ "GoldenYears". Archived from the original on 2012-02-19. Retrieved 2010-02-27.
- ^ "E-40 image". Retrieved 2011-10-13.