Pützer Elster

The Pützer Elster was a German single-engined light aircraft, manufactured by Alfons Pützer KG (later Sportavia) in Bonn. It served with the Luftwaffe and Marineflieger and was used solely for recreational sport flying. Some continue to fly in 2020 in private ownership.

Pützer Elster
Pützer Elster B
Role Light recreational aircraft
Manufacturer Pützer
Designer Alfons Pützer
First flight 10 January 1959
Status In civilian use
Primary user Luftwaffe
Number built 45
Developed from Pützer Doppelraab, Pützer Motorraab

Development history

The Pützer Elster "Magpie" was developed from the Motorraab motor glider which had itself been developed from the Doppelraab glider. The Elster was the first aircraft produced in Germany after World War II in any significant numbers. The design shared the wing of the Doppelraab, braced by metal struts, but was given a new monocoque fuselage constructed of plywood with seats for two occupants arranged side by side. The tricycle landing gear unusually featured a steerable nosewheel controlled by a hand grip. Production ceased in 1967, by which time 45 examples had been built.[1]

Variants
Elster B of Luftwaffe, Pferdsfeld air base 1972

Elster
Prototype aircraft fitted with a 52 hp Porsche 678/3 engine, first flight 10 January 1959.

Elster B
Elster of Luftwaffe used as glider tug, Pferdsfeld air base 1972
Main production version fitted with a 95 hp Continental C-90 engine. 25 aircraft were operated by the Luftwaffe and Marineflieger sport flying groups. These aircraft were initially operated with civilian registrations but were allocated military serials in 1971.[2] In 1978 the maintenance contract with Pützer expired and the aircraft were placed on the civil market.

Elster C
The Elster C was fitted with the more powerful 150 hp Lycoming O-320 engine and other modifications for use as a glider tug.

Operators

Military operators
 Germany

Specifications (Pützer Elster B)

Data from Jane's All the World's Aircraft 1962-63[3]

General characteristics

  • Crew: 1
  • Capacity: 1 pax / student
  • Length: 7.1 m (23 ft 4 in)
  • Wingspan: 13.22 m (43 ft 4 in)
  • Height: 2.5 m (8 ft 2 in)
  • Wing area: 17.5 m2 (188 sq ft)
  • Empty weight: 460 kg (1,014 lb)
  • Max takeoff weight: 700 kg (1,543 lb)
  • Fuel capacity: 64 L (17 US gal; 14 imp gal) in two tanks aft of the seats
  • Powerplant: 1 × Continental C90-12F 4-cylinder air-cooled horizontally-opposed piston engine, 71 kW (95 hp)
  • Propellers: 2-bladed Hoffmann, 1.83 m (6 ft 0 in) diameter wooden fixed-pitch propeller

Performance

  • Maximum speed: 168 km/h (104 mph, 91 kn) at sea level
  • Cruise speed: 150 km/h (93 mph, 81 kn)
  • Stall speed: 74 km/h (46 mph, 40 kn)
  • Never exceed speed: 180 km/h (110 mph, 97 kn)
  • Range: 450 km (280 mi, 240 nmi)
  • Service ceiling: 5,000 m (16,000 ft) ~
  • Rate of climb: 3.7 m/s (720 ft/min)
  • Wing loading: 38.9 kg/m2 (8.0 lb/sq ft)
  • Power/mass: 0.1011 kW/kg (0.0615 hp/lb)
  • Take-off distance to 15 m (49 ft): 240 m (787 ft)
  • Landing distance from 15 m (49 ft): 190 m (623 ft)

See also

Aircraft of comparable role, configuration, and era

References
  1. Green p.32. 1964
  2. Jackson p.134. 1976
  3. Taylor, John W.R., ed. (1962). Jane's All the World's Aircraft 1962-63. London: Sampson Low, Marston & Co. p. 68.

Further reading
  • Jackson, Paul A. (1976). German military aviation, 1956-1976. Hinckley, Leicestershire, UK: Midland Counties Publications. ISBN 0-904597-03-2.
  • Green, William (1964). The Macdonald aircraft handbook. London: Doubleday / Macdonald & Co. (Publishers) Ltd.
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