Rohrbach Ro.V Rocco

Werk Nr 26 was flown by Severa GmbH for comparison flights with the Dornier Super Wal, then latter as a seaplane trainer.

The one aircraft was built in 1927, and was used by Lufthansa between 21st May and 15th June 1928 for 47 flights between Travemunde and Oslo via Copenhagen and Gothenburg after this it was delivered to the Erpobungstelle at Travemunde.

Ro V Rocco
Engines: 2 x Rolls-Royce Condor, 480kW
Wingspan: 26.0 m / 85 ft 4 in
Length: 19.3 m / 63 ft 4 in
Height: 6.7 m / 22 ft 0 in
Wing area: 94.0 sq.m / 1011.81 sq ft
Max take-off weight: 9600 kg / 21164 lb
Empty weight: 5990 kg / 13206 lb
Max. speed: 220 km/h / 137 mph
Cruise speed: 168 km/h / 104 mph
Ceiling: 3150 m / 10350 ft
Range w/max.fuel: 2400 km / 1491 miles
Crew: 3
Passengers: 10

Rohrbach Ro V Rocco

Rohrbach

Rohrbach Metall Flugzeugbau GmbH
Rohrbach-Metall-Aeroplane Co A/S

Rohrbach Metall Flugzeugbau GmbH was founded in 1922 by Dr. Ing. Rohrbach to continue construction and development of all-metal aircraft designed by him when working previously with the Zeppelin company. Associated company, Rohrbach-Metall-Aeroplane Co A/S, formed in Copenhagen to avoid limitations imposed on construction in Germany.

Built ten Ro-ll seaplanes for Japanese Navy and Ro-IIIA for Turkey, followed by Rodra twin-engine flying-boat and Rofix single-seat fighter. Copenhagen plant closed in late 1920s when restrictions on German manufacture were lifted. German factory continued flying-boat and landplane construction, including Roland three-engined 10-passenger monoplane.

In April 1934 Weser Flugzeugbau GmbH took over the company and Dr. Rohrbach became technical director of Weser.

Rogožarski AŽR

The Rogožarski AŽR (Serbian Cyrillic: Рогожарски АЖР) was a single-engined, two-seat biplane aircraft designed as a trainer in Yugoslavia before World War II. It was designed by Viljem Šuster and built at the Rogožarski factory in Belgrade.

The aircraft was a biplane with the lower wing smaller than the upper. It was equipped with a seven-cylinder Walter Castor air-cooled radial engine of 240 hp and a wooden double-bladed propeller. The plane had dual controls, the two crew (pilot and flight instructor), sat one behind the other. It was to be employed as an intermediate trainer, replacing the outdated Hansa-Brandenburg C.I. The fuselage, which was of rectangular cross-section, was made of wood and covered with plywood. The wings had rounded ends, each was connected by a pair of metal struts and wire tensioners. Construction of the wing involved the use of wood covered with canvas. The landing gear was fixed and had no axle.

The first flight was conducted by a factory test pilot on November 5, 1930 and after the completion of factory tests, was handed over to the Yugoslav Royal Air Force Commission for testing.

The AZR was planned to replace the obsolete Hansa Brandenburg aircraft in the future. However, the flight characteristics were lower than the requirements, and they refused mass production.

The aircraft was only used in 1931 for advertising purposes, demonstration flights and participation in air shows. It also competed in the King’s Cup and the like; AZR still hoped to come to some arrangement with the military. This did not happen, Rogozarski withdrew from aircraft design, the prototype was registered as a civilian plane and used by the factory. It received the civil registration UN-PAU. In the meantime, the economic situation was such that the AŽR was standing in its hangar, waiting for better days; despite bank loans, there was a distinct lack of orders and the company went bankrupt in 1933.

Circumstances improved in the summer of 1934 when the Yugoslav Air Force bought the AZR and the fortunes of the factory improved, becoming a shareholder company. The AŽR was used as a trainer until 1937.

Engine: 1 × Walter Castor 7-cyl radial, 176 kW (236 hp)
Propellers: 2-bladed
Wingspan: 10.55 m (34 ft 7 in)
Wing area: 27.00 sq.m (290.6 sq ft)
Length: 7.55 m (24 ft 9 in)
Height: 3.05 m (10 ft 0 in)
Empty weight: 859 kg (1,894 lb)
Gross weight: 1,433 kg (3,159 lb)
Maximum speed: 215 km / h
Cruising speed: 185 km / h
Range: 745 km (463 mi; 402 nmi)
Service ceiling: 5,320 m (17,450 ft)
Rate of climb: 4.78 m/s (941 ft/min)
Crew: 2

Rogožarski SIM-II

Engine: Siemens Sh 14, 82 kW (110 hp)
Propeller: 2-blade
Wingspan: 12.40 m (40 ft 8 in)
Wing area: 21.70 sqm (233.6 sq ft)
Length: 7.80 m (25 ft 7 in)
Height: 2.68 m (8 ft 10 in)
Empty weight: 520 kg (1,146 lb)
Gross weight: 770 kg (1,698 lb)
Maximum speed: 105 km/h (65 mph; 57 kn) 148 km/h at sea level
Range: 750 km (466 mi; 405 nmi)
Service ceiling: 5,000 m (16,404 ft)
Crew: 2

Rogožarski SIM-XV / R-313

In connection with the growing danger of war in the second half of the thirties Yugoslavia started to carry out intensive work on designing new types of modern combat aircraft. Specifically, multi-purpose aircraft, which can be used as a light bomber, ground-attack aircraft and tactical explorer. Work to meet these requirements was begun by Ikarus and Rogožarskij.

In 1937 Rogožarski (Prva srpska fabrika aeroplana Rogožarski – Прва српска фабрика аероплана Живојин Рогожарски А. Д.) established a working group of engineer to proceed the project of a light twin-engine battle aircraft, designated R-313.

The Rogozarski R-313 (Рогожарски Р-313 in Serbian), originally called SIM-XV, was a two-seater twin-engined monoplane fighter/light bomber/reconnaissance aircraft. It was powered by two in-line Walter Sagitta IIR engines, both fitted with a compressor; each was capable of 493 hp. The inner fuel tank held 680 litres. The elliptical, wooden fuselage was covered in plywood which was also used to ‘skin’ the round-tipped, trapezoidal wings. The engine nacelles also housed the landing gear. The tail-wheel was, like the main landing gear, retractable. The fuel tank was located in the centre section between the wings. The reconnaissance variant of this aircraft was due to be equipped with a camera, a radio, a fixed 20mm cannon and a single FN 7.9mm machine gun, flexibly mounted. As a light bomber, the plane would carry four 106 kg ‘Stankovic’ bombs inside the fuselage. It was designed and built at the Rogozarski factory in Belgrade.

Construction of the prototype began in 1938 and completed at the end of next year. According to various sources, the first flight of the R-313 took place either at the end of 1939 or in July 1940. A total of 25 aircraft were planned, both reconnaissance and light bomber versions. In any case, the Sturmovik for the most part justified the hopes of the Air Force, whose specialists noted only the insufficient power of the engines. The engineers responded to the military’s wishes, presenting soon the variants of the R-313 with Daimler-Benz DB-601 and Rolls-Royce Merlin engines. Both versions brought the aircraft to the level of foreign aircraft, but because of the German invasion of a number of European countries, deliveries of foreign-made engines became not possible.

The prototype became part of 603 training squadron which was located at Grab, near Trebinje during the April war. It was damaged and abandoned attempting to take-off from Grab on 12 April 1941. A month later, the Germans took control and sold the machine to the Croats who had taken over the ‘Ikarus’ factory. They renamed the aircraft “Независни” (“Independent”); after repairs, a test flight was carried out on 19 May 1942. Sabotage was then detected, so serious that further repairs could not be carried out. Thus ended the plane which was popular in literature as the “Yugoslav moskito” Although it was designed and built long before its legendary counterpart.

Crew: 2
Engines: 2 × Walter Sagitta I-SR, 368 kW (493 hp) each
Propellers: 3-bladed Ratier
Wingspan: 13.00 m (42 ft 8 in)
Wing area: 26.40 m2 (284.2 sq ft)
Length: 11.00 m (36 ft 1 in)
Height: 2.68 m (8 ft 10 in)
Empty weight: 2,950 kg (6,504 lb)
Gross weight: 4,270 kg (9,414 lb)
Maximum speed SL: 376 km/h (234 mph; 203 kn)
Maximum speed 4000m/13,123ft: 460 km/h / 286 mph
Range: 1,000 km (621 mi; 540 nmi)
Service ceiling: 8,000 m (26,000 ft)
Rate of climb: 8.33 m/s (1,640 ft/min)
Time to 3000m / 10,000 ft: 5,7 min
Armament: 1x 20 mm (Oerlikon FF) HS-404 cannon, 1x flexible 7,92 mm Browning FN machine gun
Bombload: 400 kg / 882 lb