Aérospatiale SA 360 Dauphin
|SA 360 Dauphin|
|Aérospatiale Dauphin of the German police|
|First flight||2 June 1972|
|Number built||2 prototypes + 34 production examples|
|Developed into||Eurocopter AS365 Dauphin|
The Aérospatiale SA 360 Dauphin was a single-engine French utility helicopter developed as a replacement for Aérospatiale's Alouette III in the early 1970s and to fill a gap in the company's product line in the six to ten-seat helicopter category. However, as the new helicopter offered little advantage over its predecessor and thus limited market appeal, production of the SA 360 Dauphin was abandoned after only a few dozen of them had been built.
Aérospatiale had also developed a twin-engine derivative, the Dauphin 2, which proved to be quite successful and has been in production for nearly 40 years. After the merger of Aérospatiale's helicopter division into Eurocopter in 1992, the Dauphin 2 designation was dropped, and Eurocopter-built Dauphin 2s are simply referred to as "Dauphin". The retronym "Dauphin 1" is sometimes applied to the original Dauphin.
Design and development
The Dauphin design was originally derived from the Alouette III it was intended to succeed, and in fact used the rotor blades from that aircraft. Power was provided by a 730 kW (980 hp) Turbomeca Astazou XVI turboshaft, in place of later Alouette IIIs' Astazou XIV. The aircraft featured a fully enclosed cabin with seating for up to nine passengers, a four-bladed main rotor and a thirteen-bladed fenestron in the tail. It was fitted with fixed, tailwheel undercarriage with spatted mainwheels. The first of two prototypes (registration F-WSQL) made its first of 180 test flights in this configuration on 2 June 1972.
Following this initial evaluation, a number of modifications were incorporated into the design. These included increasing engine power by use of an Astazou XVIIIA of 780 kW (1,050 hp), and replacement of the original rotor blades with plastic blades. Aérospatiale engineers hoped to reduce vibration and ground resonance. Thus modified, test flights resumed in May 1973, in time to present the new aircraft at that year's Paris Air Show. In the meantime, a second prototype (registration F-WSQX) joined the test programme, flying first on 29 January. At the show, the first prototype broke three world airspeed records for helicopters in the 1,750 kg - 3,000 kg class (FAI class E-1d). Piloted by Roland Coffignot and carrying a dummy payload to represent eight passengers, it broke the 100 km closed-circuit (299 km/h, 186 mph), 3 km straight-course (312 km/h, 195 mph), and 15 km straight-course (303 km/h, 189 mph) records.
Series production of the definitive SA 360C version began in 1974, with the first completed aircraft flying in April 1975. French civil certification was obtained in December that year, and deliveries to customers commenced in January 1976. In the meantime, Aérospatiale had flown the prototype Dauphin 2 nearly a year earlier, on 24 January 1975, which would ultimately prove the death-knell for the Dauphin. A helicopter of this size powered by only a single engine was perceived in the marketplace as something of an anomaly and rather under-powered, meaning that by the end of 1976, Aérospatiale was left with 15 airframes - almost half those produced to date - with no buyers. Accordingly, production was terminated the following year.
A single airframe (Construction Number 1012, registration F-WZAK). was modified by Aérospatiale from standard SA 360C configuration to develop a version optimised for hot-and-high conditions, designated SA 360H. The main differences were the use of a 1,040 kW (1,400 hp) Astazou XXB engine and the Starflex rotorhead that had been developed for the Ecureuil. Deciding that the main customers for this more powerful aircraft were likely to be military ones, the aircraft was further modified and re-designated SA 360HCL (Helicoptere de Combat Leger - "Light Combat Helicopter"). It was fitted with a SFIM APX M397 roof-mounted, gyro-stabilised sight, and a nose-mounted sensor package incorporating a SFIM Vénus night-vision system and TRT Hector thermal-vision system. Armament consisted of eight launcher tubes for Euromissile HOT missiles, with options to carry most of the armament packages used by the Gazelle. So equipped, it could carry thirteen combat-ready troops into battle, or be used in the area neutralisation or anti-tank role. This aircraft was taken on by the Armée de Terre for evaluation, but no production order ensued.
- SA 360 - two prototypes
- SA 360C - standard production version, 34 built
- SA 360A - navalised version for Aeronavale, 1 converted from SA 360C.
- SA 361H - "hot and high" version with more powerful (969 kW (1,300 shp)) Astazou XX engine, glassfibre rotor blades and new rotor hub. Three converted from SA 360 and 360C.
- SA 361HCL - militarised version, 1 converted from SA 361H.
- One Dauphin (Construction number 1028, Registration RP-C220) was destroyed in an accident while filming Delta Force 2: The Colombian Connection. Four members of the film crew were killed, in addition to the pilot.
- One SA 360C (Construction number 1006, Registration N49505) crashed in the water during take-off from Laguardia Airport, NY, due to loss of engine power on 04/26/1985. Seven persons managed to evacuate the helicopter as it rolled over and sank, but one passenger was trapped and drowned with his seat belts still fastened.
Specifications (SA 360C Dauphin)
Data from To the throne...on its third try
- Crew: 1 or 2 pilots
- Capacity: 8-9 passengers
- Length: 13.20 m (43 ft 3¾ in)
- Rotor diameter: 11.50 m (37 ft 8¾ in)
- Height: 3.50 m (11 ft 5¾ in)
- Disc area: 103.9 m² (1,118 ft²)
- Empty weight: 1,580 kg (3,483 lb)
- Max. takeoff weight: 3,000 kg (6,614 lb)
- Powerplant: 1 × Turbomeca Astazou XVIIIA turboshaft, 783 kW (1,050 shp)
- Never exceed speed: 315 km/h (170 knots, 197 mph)
- Cruise speed: 274 km/h (148 knots, 170 mph)
- Range: 675 km (365 nmi, 419 mi) (max fuel)
- Service ceiling: 4,600 m (15,100 ft)
- Rate of climb: 9.0 m/s (1,770 ft/min)
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
- Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing. p. 16.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 889 Sheet 25.
- Apostolo, Giorgio (1984). The Illustrated Encyclopedia of Helicopters. New York: Bonanza.
- "airliners.net". Retrieved 2007-04-28.
- Lenton, Lenny. "Copter Crazy". Archived from the original on August 22, 2004. Retrieved 2007-04-28.
- "airwar.ru". Retrieved 2007-04-28.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 36.
- Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing. p. 25.
- Francillon and McKenzie Air International July 1995, p. 15.
- "World Air Forces 1981". flightglobal.com. Retrieved 15 February 2014.
- "New York airports helo link set to go". flightglobal.com. 3 January 1981. Retrieved 15 February 2014.
- "National Transportation Safety Board Accident Report DCA85AA020". Retrieved 2009-11-05.
- Francillon and McKenzie Air International July 1995, p. 16.
- (overall length), 10.98 m (36 ft 0⅓ in) (fuselage length)
- Francillon, René J. and Carol A McKenzie. "To the throne...on its third try: Dauphin, eldest son of King Alouette III". Air International, July 1995, Vol 49 No 1. pp. 14–19. ISSN 0306-5634.
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