Jump to content

User:Nimbus227/sandbox

From Wikipedia, the free encyclopedia

Specifications (Dornier Do 215 B-1)

[edit]
3-view drawing from L'Aerophile, August 1939

Data from Profile Publications 164, The Dornier Do 17 & 215 and German Aircraft of the Second World War[1][2]

General characteristics

  • Crew: 4
  • Length: 15.8 m (51 ft 10 in)
  • Wingspan: 18 m (59 ft 1 in)
  • Height: 4.56 m (15 ft 0 in)
  • Wing area: 55 m2 (590 sq ft)
  • Airfoil: root: NACA 2218; tip: NACA 2209[3]
  • Empty weight: 4,739 kg (10,448 lb)
  • Gross weight: 9,200 kg (20,283 lb)
  • Fuel capacity: 1,550 L (410 US gal; 340 imp gal) in two wing tanks + optional 875 L (231 US gal; 192 imp gal) auxiliary tank in the bomb bay
  • Powerplant: 2 × Daimler-Benz DB 601Aa V-12 inverted liquid-cooled piston engines, 820 kW (1,100 hp) each
  • Propellers: 3-bladed constant-speed propellers

Performance

  • Maximum speed: 470 km/h (290 mph, 250 kn) at 5,000 m (16,000 ft)
  • Cruise speed: 410 km/h (250 mph, 220 kn)
  • Range: 1,553 km (965 mi, 839 nmi)
  • Service ceiling: 9,500 m (31,200 ft)
  • Rate of climb: 6.0 m/s (1,180 ft/min)
  • Wing loading: 167 kg/m2 (34 lb/sq ft)
  • Power/mass: 0.178 kW/kg (0.108 hp/lb)

Armament

  • Guns: 4 × 7.92 mm (0.312 in) MG 15 machine guns, (later upgraded to 6)
  • Bombs: 1,000 kg (2,200 lb) bombs carried internally
  1. ^ Smith, J. Richard. The Dornier Do 17 & 215. Leatherhead, Surrey: Profile Publications. p. 16.
  2. ^ Smith, J.R.; Kay, Antony L. (1972). German Aircraft of the Second World War. London: Putnam. pp. 126–127. ISBN 978-0-85177-836-5.
  3. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.