The Nieuport-Delage NiD 580 R.2 was a contender for a French government contract for a long range, two-seat reconnaissance aircraft, issued in 1928. The R.2 specification called for an all-metal aircraft that was fast, climbed rapidly and had a large radius of action. The NiD 580 was a monoplane with a two-part trapezoidal parasol wing built around a central box of two interbraced spars, and a fuselage built around four longerons with an equilateral triangular section, vertex down. A Hispano-Suiza 12Nb water-cooled upright V-12 engine of 480 kilowatts powered it. There were eight prototypes in the long range reconnaissance contest held at Villacoublay in 1931 and 1932, and the NiD 580 was not selected for production, although it was shown at the 18th Paris Aero Salon in November and December 1932. The date of its first flight is not known.
Facts
Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Nieuport-Delage NiD 580 (Wikipedia)
Of Make
Source Wikipedia: Nieuport
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Source Wikipedia: NieuportAircraft producedQuote, Aircraft produced
Nieuport-Delage NiD 580 – two-seat reconnaissance parasol monoplane.
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Source Nieuport-Delage NiD 580 (Wikipedia)LeadQuote, Lead
was a contender for a French government contract for a long range, two seat reconnaissance aircraft
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1. Nieuport-Delage NiD 580 (Wikipedia)
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was a contender for a French government contract for a long range, two seat reconnaissance aircraft
Specifications, power
Powerplant: 1 × Hispano-Suiza 12Nb water-cooled, upright V-12, 480 kW (650 hp)
Specifications, empty weight
Empty weight: 1,828 kg (4,030 lb)
Specifications, gross weight
Gross weight: 2,635 kg (5,809 lb)
Specifications, maximum speed
Maximum speed: 265 km/h (165 mph, 143 kn)
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Aircraft producedQuote, Aircraft produced
Nieuport-Delage NiD 580, two-seat reconnaissance parasol monoplane.
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