Dassault MD 315 Flamant

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Flamant
Dassault Flamant Basle - September 1977.jpg
Dassault MD 312 Flamant of the Armée de l'Air at Basle, September 1977
 Tipe Military transport aircraft
 Produsen Dassault Aviation
 Terbang perdana 6 July 1947 (MD.315)
 Diperkenalkan 1948
 Dipensiunkan 1981
 Pengguna French Air Force
Vietnam Air Force
Tunisian Air Force
Cambodian Air Force

Dassault MD 315 Flamant adalah sebuah pesawat transportasi ringan bermesin ganda Perancis dibuat tak lama setelah Perang Dunia II oleh Dassault Aviation untuk Angkatan Udara Perancis.

Dassault M.D.315 Flamant

Daftar isi

  • 1 Varian
  • 2 Operator
  • 3 Spesifikasi (Flamant)
    • 3.1 Ciri-ciri umum
      • Kru: 2
      • Kapasitas: 10 passengers
      • Panjang: 12.50 m
      • Lebar 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
      Kinerja
      • Laju maksimum: 300 km/h (160 knots, 190 mph)
      • Jangkauan: 1,215 km
      • Batas atas layanan: 8,000 m
      • Power/massa: 147 W/kg (0.0897 hp/lb)
      Lihat pula
    • 3.2 Daftar yang berhubungan
      • List of military transport aircraft
      • List of military aircraft of France
      Referensi

Varian [sunting]

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]

 Kamboja
 Kamerun
 Perancis
 Madagaskar
 South Vietnam
 Tunisia

Spesifikasi (Flamant) [sunting]

Ciri-ciri umum

  • Kru: 2
  • Kapasitas: 10 passengers
  • Panjang: 12.50 m
  • Lebar 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:Renault 12S 02-201 inline piston, 433 kW

Kinerja

Lihat pula

Daftar yang berhubungan

Referensi

Catatan
Bibliografi
  • Bridgman, Leonard (ed.) Jane's All The World's Aircraft 1953-54. London:Jane's, 1953.