| SA 360 Dauphin | |
|---|---|
.jpg) Aérospatiale SA365C2 Dauphin of the Germanpolice | |
| General information | |
| Type | Utility helicopter |
| National origin | France |
| Manufacturer | Aérospatiale |
| Number built | 2 prototypes + 34 production examples |
| History | |
| Manufactured | 1976–77 |
| Introduction date | 1976 |
| First flight | 2 June1972 |
| Developed into | Eurocopter AS365 Dauphin |
TheAérospatiale SA 360 Dauphin is a single-engine Frenchutility helicopter that was developed and produced byaerospace manufacturerAérospatiale.
Developed during the early 1970s as a replacement for the company'sAlouette III helicopter, as well as to fill in an apparent gap in the company's existing product line, falling within the six to ten-seat helicopter category. Performing itsmaiden flight on 2 June 1972, the prototypes demonstrated the type's performance capacities by setting three world airspeed records for helicopters in the 1,750 kg – 3,000 kg class. The Dauphin was marketed towards both civilian and military customers.
Production of the SA 360 Dauphin was cancelled after the production run had been completed. Aérospatiale adapted the design into a twin-engine derivative of the SA 360, theDauphin 2, which proved to be commercially successful, having been in production for in excess of 40 years.
During the 1960s, French aircraft companySud Aviation, which merged intoaerospace manufacturerAérospatiale at the end of the decade, had developed a broad range of rotorcraft, including theGazelle, a fast scout/light attack helicopter, and thePuma, a medium-sized utility helicopter.[1] Towards the end of that decade, the company recognised that there was a vacant slot between the smaller Gazelle and the larger Puma for which a new helicopter could be developed to fulfil. Accordingly, during the early 1970s, Aérospatiale undertook a project to develop such a rotorcraft, resulting in theSA 360 Dauphin.[2]
On 2 June1972, the first of two Dauphin prototypes (registrationF-WSQL) performed the first of 180 test flights in its original configuration.[3][4] It was initially powered by a singleTurbomeca Astazou XVIturboshaft engine, capable of generating up to 730 kW (980 hp) of thrust. The original design of the Dauphin drew heavily upon several of Aérospatiale's other rotorcraft, having adopted thefenestronanti-torque device of the Gazelle and the main rotor system of theAlouette III.[2] Following an initial period of evaluation, a number of modifications were incorporated onto the prototypes. These included an increase of engine power with the adoption of the more powerfulAstazou XVIIIA powerplant, capable of generating up to 780 kW (1,050 hp). Additionally, the original metal rotor blades were replaced with composite versions, Aérospatiale engineers had made this change for the purpose of reducing both vibration levels and instances ofground resonance.[4]
Post modifications, the test flights resumed in May1973, in time to present the new aircraft at that year'sParis Air Show. In the meantime, a second prototype (registrationF-WSQX) joined the test programme, flying first on 29 January.[3] 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, while 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.[4]
Series production of the definitiveSA 360C version was started in 1974;[4] the first completed aircraft made its first flight during April 1975.[5] French civil certification was obtained in December that year,[3] while deliveries to customers commenced during January 1976.[3] In the meantime, Aérospatiale had flown the prototype of the improvedDauphin 2 nearly a year prior to this, on 24 January 1975;[3][2] which would ultimately prove the death-knell for the original Dauphin model. A helicopter of this size that was 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.[4][6] Accordingly, production of the type was end the following year, being replaced almost immediately by the twin-enginedAS365 Dauphin.[7][6]
A single airframe (Construction Number 1012, registrationF-WZAK) was modified by Aérospatiale from the standard SA 360C configuration into a new version,[7] which was optimised for hot-and-high conditions, designatedSA 360H. The major differences from its former configuration were the installation of an even more powerful Astazou XXB engine, capable of providing up to 1,040 kW (1,400 hp), along with the adoption of theStarflexrotorhead which had been originally developed for theAérospatiale AS350 Écureuil helicopter.[3]
The company subsequently decided that the most likely customers for this more powerful model would to be military air arms, thus the sole rotorcraft was further modified and re-designatedSA 360HCL (Helicoptere de Combat Leger – "Light Combat Helicopter").[4] In this configuration, it was outfitted with aSFIM APX M397 roof-mounted,gyro-stabilised sight, and a nose-mounted sensor package incorporating aSFIM Vénus night-vision system andTRT Hector thermal-vision system.[8] Armament consisted of eight launcher tubes forEuromissile HOT missiles, with options to carry most of the armament packages used by the lighterGazelle helicopter.[4] Thus equipped, the SA 360HCL could carry thirteen combat-ready troops into battle, as well as be used in the area neutralisation or anti-tank role.[9] This sole rotorcraft was taken on by theArmée de Terre for evaluation purposes, but no production order ever followed for the type.[3]
The Aérospatiale SA 360 Dauphin was a single-engine French utility helicopter. Much of its design was originally derived from theAlouette III that the Dauphin had been developed as a successor to, and thus shares many features, such as the rotor blades of its four-bladed main rotor, with this earlier rotorcraft.[10] The majority of Dauphins were powered by a singleAstazou XVIIIA powerplant, capable of generating up to 780 kW (1,050 hp) of thrust; this powerplant had been derived from the Astazou XIV engine that powered the latter-built examples of the Alouette III family. The Dauphin featured a fully enclosed cabin while could be provisioned with seating for a maximum of nine passengers. It was fitted with a fixed tailwheelundercarriage with spatted mainwheels; this arrangement was reportedly a source of difficulties while landing on compact helipads.[11]
One of the Dauphin's more noticeable innovations over the Alouette III was the adoption of a thirteen-bladedfenestronanti-torque device embedded within its tail.[12][13] While the fenestron had been first introduced a few years earlier upon another of Aérospatiale's rotorcraft, theGazelle, the Dauphin's implementation featured considerable refinement over the earlier arrangement; the direction of rotation was reversed so that the blade on the bottom was the advancing blade, the original direction having proved unfavourable when encountering the downwash of the main rotor during early testing of the Dauphin. Testing demonstrated the fenestron to have clear performance advantages over the conventional tail rotor, leading to it being applied to numerous other rotorcraft following the Dauphin as well.[12]
According to aviation author J. Mac McClellan, even in its original guise, the flying qualities of the Dauphin were generally appreciated by pilots.[11] One small area of criticism was that pilots had to enter and exit the front seats via the main cabin, as the rotorcraft lacked forward crew doors; passengers were also inconvenienced by the presence of a sizable vertical column in the center of the cabin that accommodated the main pushrods. These shortcomings were addressed in subsequent versions of the twin-engined Dauphin 2.[11]
Data fromAir International July 1995[18]
General characteristics
Performance
Related development
Aircraft of comparable role, configuration, and era
Related lists
