Kalpana Kalpana (Editor)

Siemens Schuckert R.VIII

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
125 km/h

Length
  
22 m

Wingspan
  
48 m

Manufacturer
  
Siemens-Schuckert

Siemens-Schuckert R.VIII flyingmachinesruImages7PutnamGermanGiants109

The Siemens-Schuckert R.VIII was a bomber aircraft designed and built in Germany from 1916.

Having cut their teeth with the Steffen R series, Siemens-Schuckert planned to produce a six engined Riesenflugzeug for the Military Air Service. In common with many of the other contemporary R projects the R.VIII had all six engines inside the fuselage, where they were tended by mechanics, driving two tractor and two pusher propellers mounted between the mainplanes, via leather cone clutches combining gearboxes, shafts and bevel gearboxes. Two aircraft were built but only the first, R23/16, was completed. Ground trials began in 1919, after the armistice, but were interrupted by a gearbox failure which resulted in a propeller breaking up and causing extensive damage. The second airframe, R24/16, was never completed and the first was not repaired after the ground running accident due to the Versaille Treaty restrictions. At the time of its completion the Siemens-Schuckert R.VIII was the largest complete aeroplane in the world; (the Mannesman-Poll triplane was to have been much larger but was not completed before the Versailles Treaty restrictions were applied).

Specifications (Siemens-Schuckert R.VIII)

Data from The German Giants German aircraft of the First World War

General characteristics

  • Crew: 6+
  • Length: 21.6 m (70 ft 10 in)
  • Wingspan: 48 m (157 ft 6 in)
  • Height: 7.4 m (24 ft 3 in)
  • Wing area: 440 m2 (4,700 sq ft)
  • Empty weight: 10,478 kg (23,100 lb)
  • Gross weight: 15,867 kg (34,980 lb)
  • Powerplant: 6 × Basse und Selve BuS.IVa 6-cyl. water-cooled in-line piston engines, 220 kW (300 hp) each
  • Propellers: tractor 900 rpm - 2 bladed , pusher 700 rpm - 4-bladed
  • Performance

  • Maximum speed: 125 km/h (78 mph; 67 kn) (estimated)
  • Range: 900 km (559 mi; 486 nmi) (estimated)
  • Service ceiling: 4,000 m (13,000 ft) (estimated)
  • Wing loading: 35 kg/m2 (7.2 lb/sq ft)
  • Cost - 750,000 Marks
  • References

    Siemens-Schuckert R.VIII Wikipedia