Nord Norelfe
| Norelfe | |
|---|---|
| Role | Three-seat experimental helicopter |
| National origin | France |
| Manufacturer | Nord Aviation |
| Designer | Jean Cantinieau |
| First flight | 28 December 1954 |
| Number built | 2 |
The Nord 1750 Norelfe was a 1950s French three-seat helicopter built by Nord Aviation and designed by Jean Cantinieau.
Development
The 1750 Norelfe was based on the Matra-Cantinieau MC-101A, an earlier helicopter designed by Jean Cantinieau. It had a single main rotor, with torque control through a movable duct at the end of the tailboom. Powered by a Turbomeca Artouste turboshaft, the first of two Norelfes flew on 28 December 1954.[1]
The company sold the two helicopters and the design rights to Aerotécnica of Spain who redesignated them the Aerotécnica AC-13A.[1] Aerotécnica went on to produce a larger five-seat version, the Aerotécnica AC-14 which was used by the Ejército del Aire (Spanish Air Force).
Specifications (AC-13A)
Data from Jane's All the World's Aircraft 1958-59[2]
General characteristics
- Crew: 1
- Capacity: 2 pax
- Length: 7.48 m (24 ft 6 in)
- Height: 2.75 m (9 ft 0 in) to top of rotor pylon
- Empty weight: 575 kg (1,268 lb)
- Gross weight: 880 kg (1,940 lb)
- Fuel capacity: 115 L (30 US gal; 25 imp gal)
- Powerplant: 1 × Turbomeca Artouste I turboshaft, 130 kW (170 hp) at transmission (rated to 260 shp (194 kW))
- Main rotor diameter: 9.04 m (29 ft 8 in)
- Main rotor area: 64 m2 (690 sq ft)
Performance
- Maximum speed: 140 km/h (87 mph, 76 kn)
- Cruise speed: 124 km/h (77 mph, 67 kn)
- Range: 140–345 km (87–214 mi, 76–186 nmi)
- Service ceiling: 6,065 m (19,898 ft)
- Hover ceiling IGE: 2,650 m (8,694 ft)
- Rate of climb: 4.6 m/s (910 ft/min)
See also
Related development
Related lists
References
Further reading
- Apostolo, Giorgio (1984). The Illustrated Encyclopedia Of Helicopters. New York: Bonanza Books. ISBN 978-0517439357.