Dassault MD 315 Flamant
Tampilan
![]() Dassault MD 312 Flamant of the Armée de l'Air at Basle, September 1977 | |
Tipe | Military transport aircraft |
---|---|
Terbang perdana | 6 July 1947 (MD.315) |
Diperkenalkan | 1948 |
Dipensiunkan | 1981 |
Pengguna utama | French Air Force |
Pengguna lain | Vietnam Air Force Tunisian Air Force Cambodian Air Force |
Dassault MD 315 Flamant adalah sebuah pesawat transportasi ringan bermesin ganda Prancis dibuat tak lama setelah Perang Dunia II oleh Dassault Aviation untuk Angkatan Udara Prancis.
![](http://178.128.105.246/cars-http-upload.wikimedia.org/wikipedia/commons/thumb/d/d4/Dassault_Flamant_silhouette.jpg/220px-Dassault_Flamant_silhouette.jpg)
Varian
[sunting | sunting sumber]- MD 303
Dassault MD 311 Flamant trainer at the Paris Air Show 2007 - Prototype, one built
- MD 311
- Bombing, navigation and photography training aircraft, 39 built.
- MD 312
- Six-seat transport and communications aircraft, 142 built.
- MD 312B
- Experimental version with heavier loaded weight, one built.
- MD 315
- 10-seat utility transport aircraft, 137 built.
- MD 316
- One MD 315 aircraft fitted with two 820-hp (611-kW) SNECMA 14X Super Mars radial piston engines.
- MD 316T
- One prototype fitted with a single-finned tail, and two 800-hp (597-kW) Wright R-1300-CB7A1 Cyclone radial piston engines.
Operator
[sunting | sunting sumber]- Cambodian Air Force (MD 315)
- Cameroon Air Force (MD 315)
- French Air Force (MD 315, MD 312, MD 311)
- French Navy (MD 312)
- Madagascar Aeronaval Force (MD 315, MD 312)
- Vietnam Air Force (MD 312, MD 315)
- Tunisian Air Force (MD 312)
Spesifikasi (Flamant)
[sunting | sunting sumber]Ciri-ciri umum
- Kru: 2
- Kapasitas: 10 passengers
- Panjang: 12.50 m
- Rentang sayap: 20.68 m
- Tinggi: 4.50 m
- Luas sayap: 47.2 m²
- Berat kosong: 4,250 kg
- Berat isi: 5,790 kg
- Berat maksimum saat lepas landas: 5,800 kg
- Mesin: 2 × Renault 12S 02-201 inline piston, 433 kW (580 hp) masing-masing
Kinerja
- Laju maksimum: 300 km/h (160 knots, 190 mph)
- Jangkauan: 1,215 km
- Langit-langit batas: 8,000 m
- Power/massa: 147 W/kg (0.0897 hp/lb)
Lihat pula
[sunting | sunting sumber]
- Daftar terkait
Referensi
[sunting | sunting sumber]- Catatan
- Bibliografi
- Bridgman, Leonard (ed.) Jane's All The World's Aircraft 1953-54. London:Jane's, 1953.