Zeppelin-Lindau Rs.III

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Rs III
Zeppelin-Lindau Rs.III profile drawing L'Aerophile August,1921.png
Role Patrol flying boat
National origin Germany
Manufacturer Zeppelin-Lindau
Designer Claudius Dornier
First flight4 November 1917 [1]
Primary user Kaiserliche Marine
Number built1
Developed from Zeppelin-Lindau Rs.II
Variants Zeppelin-Lindau Rs.IV

The Zeppelin-Lindau Rs.III (known incorrectly postwar as the Dornier Rs.III) was a large four-engined monoplane flying boat designed by Claudius Dornier and built during 1917 on the German side of Lake Constance at the Zeppelin-Lindau works.

Contents

Design and development

Although the Rs.III differed in appearance from its predecessors, it was the result of the experience gained from building and flying the Rs.I and Rs.II. The broad hull was retained as well as the push-pull tandem nacelles, but the open framework tail boom was replaced by a steel and Duralumin fuselage that sat on the centreline of the high mounted wing and the substantial tubular trusses supporting the wing were replaced by conventional wire bracing. [1]

The short and broad hull accommodating the flight crew supported the engine nacelles and the wing centre section on a frame-work of struts, in similar fashion to the later version of the Rs.II. The high set fuselage had several tasks, providing gun positions for defence, ensuring that the tail unit was as high as possible to reduce damage from spray and to act as a king-post for the wings landing-wire bracing. Constructed of steel longerons riveted to Duralumin frames and covered with Duralumin sheet over the forward portion and fabric aft it supported the tail unit which consisted of a biplane tail cellule with elevators and a large central rudder, initially with a long central fin, but later with two smaller fixed fins in the tail cellule. At approximately the mid-wing chord position the fuselage had a cockpit with provision for two machine guns and also housed a sound-proof wireless cabin in the nose. [1]

The hull was very similar to that of the Rs.II, being short and broad with a cockpit near the nose protected by a large coaming. Fuel for the engines was housed in a large fuel tank mounted in the hull, which also provided accommodation for the crew when not at their stations. The flight crew usually consisted of two pilots, a commander, and possibly a navigator, with gunners and mechanics to man the guns and engines as well as manually pump fuel up to each engine's gravity tanks. [1]

Operational history

As the Rs.III neared completion, the facilities at the Norderney Seaplane station on the North Sea coast were also completed. Delivery of the Rs.III was planned to follow the river Rhine after crossing the Black Forest, with a fighter escort between Rottweil and Duisburg due to the proximity of Allied forces, as well as a guide aircraft to prevent it inadvertently crossing the Dutch border. [1]

Flight testing of the Rs.III carried on apace from November 1917, at the Lake Constance factory, with good results. Flying characteristics were generally good, the aircraft proving easy to fly, taxi on water, and capable of taking off in moderate seas. With only minor modifications, the Rs.III was ready for its delivery flight by the end of January 1918, but the route was covered with fog. The weather cleared by 19 February when the Rs.III set off on its 7-hour non-stop delivery flight to Norderney. [1]

Operational testing at Norderney cleared the giant Rs.III for service with the Imperial German Navy on 13 June 1918 and it was turned over to the Seaplane Experimental Command (Seeflugzeug-Versuchs-Kommando) on 27 August 1918 for further Navy tests. After the Armistice the Rs.III was not destroyed immediately but continued flying with the German Navy Air Service on mine clearing duties until the Allied Control Commission finally ordered its scrapping in July 1921. [1]

The Rs.III had proved easy to fly (but with some minor quirks), easy to manoeuvre on the water and durable, due to its metal construction. [1]

Specifications (Rs.III)

Data from The German Giants [1]

General characteristics

Performance

Armament

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References

Notes

  1. 1 2 3 4 5 6 7 8 9 Haddow & Grosz, pp. 117–124

Bibliography

Further reading