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
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
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 developmentQuote, 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)LeadQuote, 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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