SNCASE SE.3200 Frelon
| SE.3200 Frelon | |
|---|---|
| Role | Military transport helicopter |
| National origin | France |
| Manufacturer | SNCASE Sud Aviation |
| First flight | 10 June 1959 |
| Number built | 2 |
| Developed into | Aérospatiale SA 321 Super Frelon |
The SNCASE SE.3200 Frelon (Hornet) is a French helicopter built in the late 1950s. Intended to serve as a multirole helicopter for the French Army, Air Forces and Navy, two prototypes were built and flown before the project was dropped in favour of the SA 3210 Super Frelon.[1]
Design and development
The SNCASE SE.3200 Frelon was a heavy helicopter designed to equip the French Armed Forces, replacing the Sikorsky S-58 built under license by SNCASE (Société nationale des constructions aéronautiques du Sud-Est).
The specifications called for an aircraft of less than 5 tonnes gross weight. The prototypes were powered by three Turbomeca Turmo IIIB 750/800 shp turbines to avoid all risk of engine failure: production aircraft were to have used the 1000 hp Turmo IIC. The engines drove a single four blade rotor.[2]
Fuel was held in two large external tanks having a capacity of 1100 liters each. This left the fuselage clear for large loads. The rear fuselage was a swing-tailed unit, which opened to provide clear entry for payloads such as vehicles.[1] The Frelon was able to carry light vehicles, up to 24 fully equipped troops, or 15 stretchers and two attendants if used as an air ambulance. It was equipped with a fixed tricycle landing gear.[3][unreliable source?]
Only two prototypes were built, the first one flying on 10 June 1959 at Paris – Le Bourget Airport.
Specifications
General characteristics
- Length: 15.19 m (49 ft 10 in) with rotor folded
- Empty weight: 4,500 kg (9,920 lb)
- Gross weight: 7,498 kg (16,530 lb)
- Max takeoff weight: Lua error in Module:Convert at line 272: attempt to index local 'cat' (a nil value).
- Powerplant: 3 × Turbomeca Turmo IIIB , 520 kW (700 hp) each
- Main rotor diameter: 14.99 m (49 ft 2 in)
- Main rotor diameter: 14.99 m (49 ft 2 in)
Performance
- Maximum speed: 246 km/h; 133 kn (153 mph)
- Cruise speed: 232 km/h; 125 kn (144 mph)
- Ferry range: 1,296 km; 806 mi (700 nmi)
- Service ceiling: 4,694 m (15,400 ft) at all-up weight of 5647 kg (12,450 lbs)
See also
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
References
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Wikimedia Commons has media related to SNCASE helicopters. |
- ↑ 1.0 1.1 Munson, K.; "Helicopters: and Other Rotorcraft Since 1907", revised Edition, Blandford (1973), Page 159
- ↑ 2.0 2.1 Frelon SE.3200 Flight 27 May 1960
- ↑ http://aerostories.free.fr/giravia/helico/liron/liron04/ in French
- ↑ Sud Frelon Progress Flight 8 July 1960
