Morane-Saulnier H

Morane-Saulnier H
Type H
Morane Saulnier Type H on display at the Musee de l'Air et de l'Espace at Paris Le Bourget airport
Role Sport aircraft
Manufacturer Morane-Saulnier
First flight 1913

The Morane-Saulnier H was a sport aircraft produced in France in the years before the First World War,[1][2] a single-seat derivative of the successful Morane-Saulnier G with a slightly reduced wingspan[2] Like the Type G, it was a successful sporting type in its day.

During the second international aero meet, held at Wiener Neustadt in June 1913, Roland Garros won the precision landing prize in a Type H.[3]

The French Army ordered a batch of 26 aircraft, and the British Royal Flying Corps also acquired a small number, these latter machines purchased from Grahame-White, who was manufacturing the type in the UK under licence.[2] The French machines saw limited service in the opening stages of World War I, with pilots engaging in aerial combat using revolvers and carbines.[2]

The type was also produced under licence in Germany by Pfalz Flugzeugwerke, who built it as the E.I, E.II, E.IV, E.V, and E.VI, with increasingly powerful engines.[4][5] These were armed with a single, synchronised LMG 08/15 machine gun.[4][5]

A Type H is preserved at the Musée de l'Air et de l'Espace in Le Bourget.

Variants

Pfalz-built versions

  • E.I - with Oberursel U.0 rotary engine (60 built)[4]
  • E.II - with Oberursel U.I rotary engine [4]
  • E.IV - with Oberursel U.III rotary engine (ca. 24 built)[4]
  • E.V - with Mercedes D.I water-cooled, inline engine[4]
  • E.VI - with Oberursel U.I engine, lengthened fuselage, enlarged tail fin and additional bracing (20 built)[6]

Operators

 France
  • Aéronautique Militaire
 Austria-Hungary
 Germany
 Portugal
One aircraft only.
 United Kingdom

Specifications

Data from flugzeuginfo.net

General characteristics

  • Crew: One pilot
  • Length: 5.84 m (19 ft 2 in)
  • Wingspan: 9.12 m (29 ft 11 in)
  • Height: 2.26 m (7 ft 5 in)
  • Empty weight: 188 kg (415 lb)
  • Gross weight: 444 kg (979 lb)
  • Powerplant: 1 × Le Rhône 9C, 60 kW (80 hp)

Performance

  • Maximum speed: 120 km/h (75 mph)
  • Range: 177 km (111 miles)

Notes

  1. ^ Taylor 1989, p.648
  2. ^ a b c d "The Illustrated Encyclopedia of Aircraft", p.2539
  3. ^ Hartmann 2001, 11
  4. ^ a b c d e f The Illustrated Encyclopedia of Aircraft, p.2698
  5. ^ a b Grosz 1996
  6. ^ Grosz 1996, p.27

References


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