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Heinkel HE 1

The Heinkel HE 1 (aka Caspar S 1) was a two-seat, low-wing monoplane floatplane, designed in 1921 by German designer Ernst Heinkel at Caspar-Werke.

HE 1
Role Reconnaissance floatplane
National origin Germany
Manufacturer Caspar-Werke
Designer Ernst Heinkel
First flight 1923
Primary user Swedish Navy (Marinen )
Number built 14

The HE 1 was produced under licence in Sweden for the Marinen (Swedish Navy) in 1921 as the Svenska S.2. The HE 1 was powered by a 179 kW (240 hp) Maybach Mb.IVa engine; one test aircraft was powered by a Siddeley Puma engine.

Specifications Edit

Data from [1]

General characteristics

  • Crew: Two (pilot & observer/gunner)
  • Length: 12.65 m (41 ft 6 in)
  • Wingspan: 18 m (59 ft 1 in)
  • Height: 3.85 m (12 ft 8 in)
  • Empty weight: 1,700 kg (3,748 lb)
  • Gross weight: 2,320 kg (5,115 lb)
  • Powerplant: 1 × Maybach Mb IVa 6-cylinder water-cooled inline piston engine, 190 kW (260 hp)

Performance

  • Maximum speed: 160 km/h (99 mph, 86 kn)
  • Service ceiling: 4,000 m (13,000 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 9 minutes

Armament
1 × flexible machine gun in rear cockpit

Operators Edit

  Sweden

References Edit

  1. ^ "Caspar S 1". Histaviation.com. Retrieved 27 February 2019.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 498.

heinkel, caspar, seat, wing, monoplane, floatplane, designed, 1921, german, designer, ernst, heinkel, caspar, werke, 1role, reconnaissance, floatplanenational, origin, germanymanufacturer, caspar, werkedesigner, ernst, heinkelfirst, flight, 1923primary, user, . The Heinkel HE 1 aka Caspar S 1 was a two seat low wing monoplane floatplane designed in 1921 by German designer Ernst Heinkel at Caspar Werke HE 1Role Reconnaissance floatplaneNational origin GermanyManufacturer Caspar WerkeDesigner Ernst HeinkelFirst flight 1923Primary user Swedish Navy Marinen Number built 14The HE 1 was produced under licence in Sweden for the Marinen Swedish Navy in 1921 as the Svenska S 2 The HE 1 was powered by a 179 kW 240 hp Maybach Mb IVa engine one test aircraft was powered by a Siddeley Puma engine Specifications EditData from 1 General characteristicsCrew Two pilot amp observer gunner Length 12 65 m 41 ft 6 in Wingspan 18 m 59 ft 1 in Height 3 85 m 12 ft 8 in Empty weight 1 700 kg 3 748 lb Gross weight 2 320 kg 5 115 lb Powerplant 1 Maybach Mb IVa 6 cylinder water cooled inline piston engine 190 kW 260 hp Performance Maximum speed 160 km h 99 mph 86 kn Service ceiling 4 000 m 13 000 ft Time to altitude 1 000 m 3 300 ft in 9 minutesArmament 1 flexible machine gun in rear cockpitOperators Edit SwedenSwedish Navy Swedish Air ForceReferences Edit Wikimedia Commons has media related to Heinkel HE 1 Caspar S 1 Histaviation com Retrieved 27 February 2019 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 498 Retrieved from https en wikipedia org w index php title Heinkel HE 1 amp oldid 1163391805, wikipedia, wiki, book, books, library,

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