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SPAD S.XV

Pioneer and Early Aviation Aircraft

The SPAD S.XV was a single-seat fighter designed and built in France to meet the 1918 C1 specification for a medium altitude fighter. André Herbemont of SPAD designed a single-bay, equal-span biplane with un-staggered wooden wings and a moulded plywood monocoque fuselage, powered by a 160 horsepower Gnome Monosoupape 9Nc rotary engine in a close cowling and armed with two synchronised Vickers machine guns. It first flew on 31 July 1917, but the low power of the Gnome engine limited any performance advantage over the SPAD S.XIII and production was not authorised. None were accepted by the Aviation militaire, although the monocoque fuselage idea was reused in later Herbemont designs, and a post-war sporting version was built for René Fonck and Charles Nungesser.

Facts
Year
1917 1
Engine Class
Rotary 1
Power (kW)
120 1
Top Speed (km/h)
199 1
Mass (kg)
368 1
Maximum Mass (kg)
625 1
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Exemplifies

Aviation, Modes
Source SPAD S.XV (Wikipedia)

Of Make

Source SPAD S.XV (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source SPAD S.XV (Wikipedia)Design and development
Quote, Design and development
André Herbemont, at SPAD, designed a single-bay biplane with un-staggered, equal span wooden wings and a moulded plywood monocoque fuselage.

Originated In

Also in Geography Atlas: where this subject originated.

Source SPAD S.XV (Wikipedia)Lead
Quote, Lead
The SPAD S.XV was a single-seat fighter designed and built in France and offered to fulfil a 1918 C1 specification (C1 - Chasseur single-seat).
Sources
1. SPAD S.XV (Wikipedia)
  • Design and development, first flight
    First flown on 31 July 1917
  • Specifications (S.15/2)
    Powerplant: 1 × Gnome Monosoupape 9Nc 9-cylinder air-cooled rotary piston engine, 120 kW (160 hp)
  • Specifications (S.15/2), empty weight
    Empty weight: 368 kg (811 lb)
  • Specifications (S.15/2), gross weight
    Gross weight: 625 kg (1,378 lb)
  • Specifications (S.15/2), speed
    Maximum speed: 199 km/h (124 mph, 107 kn) at 2,000 m (6,600 ft)
  • Design and development
    André Herbemont, at SPAD, designed a single-bay biplane with un-staggered, equal span wooden wings and a moulded plywood monocoque fuselage.
  • Lead
    The SPAD S.XV was a single-seat fighter designed and built in France and offered to fulfil a 1918 C1 specification (C1 - Chasseur single-seat).
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