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Antonov A-13

Antonov A-13 adalah sailplane aerobatic Soviet diterbangkan pada tahun 1950 dan 60-an. Itu kecil, satu kursi, pesawat semua logam dikembangkan dari A-11 dan opsional yang dapat dipasang dengan panjang bentang sayap pesawat. Itu adalah monoplane pertengahan sayap dengan pesawat seperti kecebong dan ekor V.

Pada bulan Februari tahun 1962, A-13 dilengkapi dengan mesin turbojet kecil untuk menciptakan rekor kecepatan udara dunia dari 196 km / h (122 mph) untuk pesawat hingga 500 kg. Versi bertenaga jet dikenal sebagai An-13

Spesifikasi

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Karakteristik umum

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  • Kru: 1
  • Panjang: 6 m (19 ft 8 in)
  • Lebar sayap: 12,1 m (39 ft 8 in)
  • Tinggi: 1,2 m (3 ft 11 in) di kokpit
  • Area sayap: 10,44 m 2 (112,4 sq ft)
  • Aspek rasio: 13.8
  • Airfoil: TsAGI R-32-15 [catatan 1]
  • Berat kosong: 254 kg (£ 560)
  • Berat kotor: 360 kg (£ 794)
  • Kecepatan Stall: 70 km / jam (43 mph, 38 kn)
  • Tidak pernah melebihi kecepatan: 350 km / h (217 mph, 189 kn)
  • Kecepatan udara Rough max: 350 km / jam (217,5 mph, 189.0 kn)
  • Aerotow speed: 200 km / jam (124,3 mph, 108.0 kn)
  • Winch kecepatan peluncuran: 120 km / jam (74,6 mph; 64,8 kn)
  • g batas: 8,66 -3.9 pada 300 km / jam (186,4 mph; 162,0 kn)
  • Maksimum meluncur rasio: 25 di 112 km / jam (69,6 mph; 60,5 kn)
  • Tingkat wastafel: 1,14 m / s (224 ft / menit) pada 97 km / jam (60,3 mph; 52,4 kn)
  • Loading sayap: 34,5 kg / m² (£ 7,1 / sq ft)

Referensi

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  • Shenstone, B.S. (1963). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (dalam bahasa Primarily English with French and German) (edisi ke-1st). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. hlm. 243–245. 
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Antonov A-13
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