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Pilatus P-5

The Pilatus P-5 was a single-engined artillery observation aircraft project from Pilatus Aircraft in Switzerland.[1]

P-5
Sketch of the Pilatus P-5
Role two-seat artillery observation aircraft
National origin Switzerland
Manufacturer Pilatus Aircraft
Number built 0

Design and development edit

External image
Pilatus P-5
  Pilatus P-5

The first drawings for the Pilatus P-5 were made in 1951. The client was the Federal Military Department (EMD). The main purpose for the P-5 was for artillery observation. It was a single-engine, two-seat high-wing monoplane with fixed wheels. The aircraft frame was intended to be built out of tubular steel and skinned with metal. The main wings and tail were intended to be made from an alloy, not steel. This aircraft had fixed wing with slats and flaps fitted on to them. The pilot and observer were seated in a generously glazed cabin that had exceptionally good visibility in all directions. This view was due mainly to the curved sides which allowed the aircrew to look almost straight down. This P-5 design was abandoned in 1951 and no prototype aircraft were ever built.[2]

Specifications (P-5 estimated) edit

Data from Pilatus Flugzeuge: 1939–1989[2]

General characteristics

  • Crew: 2
  • Length: 9.2 m (30 ft 2 in)
  • Wingspan: 12 m (39 ft 4 in)
  • Height: 2.5 m (8 ft 2 in)
  • Empty weight: 860 kg (1,896 lb)
  • Powerplant: 1 × Walter Minor 6-III I-6 inverted air-cooled piston engine, 120 kW (160 hp)

Performance

  • Maximum speed: 190 km/h (120 mph, 100 kn)
  • Landing speed: 53 km/h (33 mph; 29 kn)
  • Service ceiling: 4,800 m (15,700 ft)
  • Rate of climb: 6 m/s (1,200 ft/min)
  • Take off distance: 65 m (213 ft)
  • Landing distance: 50 m (164 ft)

See also edit

Aircraft of comparable role, configuration, and era

Notes edit

  1. ^ (PDF) (in German). Stans: Pilatus. 2011. p. 1. Archived from the original (PDF) on 2012-01-06. Retrieved 2013-05-01.
  2. ^ a b Eichenberger, Roland (1989). Pilatus Flugzeuge: 1939–1989 (in German). Stans: Pilatus Flugzeugwerk.

References edit

  • Eichenberger, Roland (1989). Pilatus Flugzeuge: 1939–1989 (in German). Stans: Pilatus Flugzeugwerk.
  • (PDF) (in German). Stans: Pilatus. 2011. p. 1. Archived from the original (PDF) on 2012-01-06. Retrieved 2013-05-01.

pilatus, single, engined, artillery, observation, aircraft, project, from, pilatus, aircraft, switzerland, 5sketch, role, seat, artillery, observation, aircraftnational, origin, switzerlandmanufacturer, pilatus, aircraftnumber, built, contents, design, develop. The Pilatus P 5 was a single engined artillery observation aircraft project from Pilatus Aircraft in Switzerland 1 P 5Sketch of the Pilatus P 5Role two seat artillery observation aircraftNational origin SwitzerlandManufacturer Pilatus AircraftNumber built 0 Contents 1 Design and development 2 Specifications P 5 estimated 3 See also 4 Notes 5 ReferencesDesign and development editExternal imagePilatus P 5 nbsp Pilatus P 5The first drawings for the Pilatus P 5 were made in 1951 The client was the Federal Military Department EMD The main purpose for the P 5 was for artillery observation It was a single engine two seat high wing monoplane with fixed wheels The aircraft frame was intended to be built out of tubular steel and skinned with metal The main wings and tail were intended to be made from an alloy not steel This aircraft had fixed wing with slats and flaps fitted on to them The pilot and observer were seated in a generously glazed cabin that had exceptionally good visibility in all directions This view was due mainly to the curved sides which allowed the aircrew to look almost straight down This P 5 design was abandoned in 1951 and no prototype aircraft were ever built 2 Specifications P 5 estimated editData from Pilatus Flugzeuge 1939 1989 2 General characteristicsCrew 2 Length 9 2 m 30 ft 2 in Wingspan 12 m 39 ft 4 in Height 2 5 m 8 ft 2 in Empty weight 860 kg 1 896 lb Powerplant 1 Walter Minor 6 III I 6 inverted air cooled piston engine 120 kW 160 hp Performance Maximum speed 190 km h 120 mph 100 kn Landing speed 53 km h 33 mph 29 kn Service ceiling 4 800 m 15 700 ft Rate of climb 6 m s 1 200 ft min Take off distance 65 m 213 ft Landing distance 50 m 164 ft See also editAircraft of comparable role configuration and era Miles MasterNotes edit Pilatus Chronik PDF in German Stans Pilatus 2011 p 1 Archived from the original PDF on 2012 01 06 Retrieved 2013 05 01 a b Eichenberger Roland 1989 Pilatus Flugzeuge 1939 1989 in German Stans Pilatus Flugzeugwerk References edit nbsp Wikimedia Commons has media related to Pilatus P 5 Eichenberger Roland 1989 Pilatus Flugzeuge 1939 1989 in German Stans Pilatus Flugzeugwerk Pilatus Chronik PDF in German Stans Pilatus 2011 p 1 Archived from the original PDF on 2012 01 06 Retrieved 2013 05 01 Retrieved from https en wikipedia org w index php title Pilatus P 5 amp oldid 1188458930, wikipedia, wiki, book, books, library,

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