Zeppelin-Lindau Rs.IV

Source: Wikipedia, the free encyclopedia.
Rs.IV
Role Patrol flying boat
National origin Germany
Manufacturer
Zeppelin-Lindau
Designer
Claudius Dornier
First flight 12 October 1918
Status scrapped
Primary user
Kaiserliche Marine
Number built 1
Developed from Zeppelin-Lindau Rs.III

The Zeppelin-Lindau Rs.IV (known incorrectly postwar as the Dornier Rs.IV) was a

Claudius Dornier while working for Zeppelin in the town of Lindau
.

Development

Two aircraft were ordered by the German

Kaiserliche Marine (Imperial Navy) in January 1918.[1] The first flight was made on 12 October 1918 and was converted shortly thereafter into a passenger aircraft sometime between October 1918, following damage sustained during its first flight, and June 1919.[1] When it was modified the pilot's position was moved to the hull instead of in the overhead fuselage in 1919. The sole completed example was scrapped on 17 April 1920 on orders from the Military Inter-Allied Commission of Control, after a detailed examination of its construction had been made; the second example was never completed.[1]

Design

Its design was based on the previous Rs.III, differing primarily in having a narrower hull fitted with

IdFlieg
in 1915) between the hull and the wing. These were staggered to allow propeller disks to overlap slightly so as to reduce adverse yaw when an engine was not running. It had the distinction of being first seaplane to have an all-metal stressed skin hull, and the first seaplane to be fitted with Dornier's patented sponsons.
[2][page needed] [3][page needed]

Operators

 German Empire
Kaiserliche Marine
- evaluation only

Specifications

L'Aerophile
, August 1921

Data from The German Giants[1]

General characteristics

  • Crew: 5
  • Capacity: (20 passengers in the commercial version)
  • Length: 22.7 m (74 ft 6 in) overall
  • Hull length: 14.2 m (46 ft 7 in)
  • Hull beam: 3.65 m (12 ft 0 in)
  • Sponson width: 8 m (26 ft 3 in)
  • Wingspan: 37.0 m (121 ft 5 in)
  • Height: 8.37 m (27 ft 6 in)
  • Wing area: 226 m2 (2,430 sq ft)
  • Empty weight: 7,237 kg (15,955 lb)
  • Gross weight: 10,600 kg (23,369 lb)
  • Fuel capacity: 3,000 L (790 US gal; 660 imp gal)
  • Powerplant: 4 × Maybach Mb.IVa 6 cylinder liquid cooled inline mounted as tandem pairs, 183 kW (245 hp) each
  • Propellers: 4-bladed wooden fixed pitch propellers, 3.1 m (10 ft 2 in) diameter

Performance

  • Maximum speed: 138 km/h (86 mph, 75 kn)
  • Minimum control speed: 90 km/h (56 mph, 49 kn)
  • Endurance: 10 hours
  • Time to altitude:
    • 400 to 800 m (1,300 to 2,600 ft) – 14 minutes
    • 400 to 1,000 m (1,300 to 3,300 ft) – 22 minutes
    • 400 to 1,400 m (1,300 to 4,600 ft) – 36.4 minutes
    • 400 to 2,000 m (1,300 to 6,600 ft) – 53.5 minutes
  • Wing loading: 46.5 kg/m2 (9.5 lb/sq ft)

See also

Related development

  • Dornier Gs.I
  • Dornier Wal

Related lists

References

Citations

  1. ^ a b c d Haddow, 1988 pp124–129
  2. ^ "The (German) Dornier "Giant Flying-Boat"". Flight. Vol. XI, no. 560. September 18, 1919. Archived from the original on 2016-03-05. Retrieved March 28, 2017 – via Flight Global.
  3. ^ "Some Dornier "Milestones" - The Do. Rs. IV, 1917-18". Flight. December 23, 1920. Retrieved March 28, 2017 – via Flight Global.

Bibliography