B Series @·AIRCRAFTUBE

  • Aviatik B.I Aviatik B.I
    Aviatik B.I
  • Aviatik Aviatik
    Aviatik
  • Aviatik B.II Aviatik B.II
    Aviatik B.II
  • Aviatik B.I Aviatik B.I
    Aviatik B.I
  • Aviatik B.I Aviatik B.I
    Aviatik B.I
  • Aviatik B.I - Navarre and S-Lt. Jean Robert first victory Aviatik B.I - Navarre and S-Lt. Jean Robert first victory
    Aviatik B.I - Navarre and S-Lt. Jean Robert first victory
  • Aviatik B.II - 1915 Aviatik B.II - 1915
    Aviatik B.II - 1915
  • Aviatik B.II Aviatik B.II
    Aviatik B.II
  • Aviatik B.II Aviatik B.II
    Aviatik B.II
  • Aviatik B.II - 1915 Aviatik B.II - 1915
    Aviatik B.II - 1915
  • Aviatik B.III - Turkish service (1922-1924) Aviatik B.III - Turkish service (1922-1924)
    Aviatik B.III - Turkish service (1922-1924)
  • Aviatik B.II Aviatik B.II
    Aviatik B.II
  • Aviatik B.II Aviatik B.II
    Aviatik B.II

Aviatik B.I

The Aviatik B.I was a German two-seat reconnaissance biplane designed and built by the Automobil und Aviatik AG company, who until then had produced copies of French designs.

The B.I was developed from a 1913 design for a racing aircraft. The crew sat in open tandem cockpits with the observer in the front. It entered service in 1914.

It was followed by the B.II model, which had a more powerful Mercedes engine and was later armed with a single 7.7 mm machine gun.

The B.I was manufactured in large numbers in Italy under licence by Società Aeronautica Meccanica Lombardia (SAML), which built 410 examples according to Aviatik's design. The firm then put two modified versions of their own into production, as designed by Robert Wild. The first of these, the SAML S.1 was powered by a Fiat A.12 engine and was armed with a Revelli machine gun for the observer. The second version, the SAML S.2 was intended for the reconnaissance-bomber role and had a shorter wingspan, a fixed, forward-firing Revelli gun in addition to the one in the rear cockpit, and a bomb load of 40 kg (90 lb). The 16 Squadriglie da Recognizione operated 660 S-1s and S-2s from 1917 onwards in Italy, Albania, and Macedonia. Two SAML S.1 participated in the Revolution of 1922 in Paraguay in the government side. They survived the conflict and they were the first planes of the new Military Aviation School, along a single SVA-5, a SVA-10 and a SPAD S.20. One S.1 was destroyed in an accident in 1928 but the other survived as a trainer during the Chaco War.

Aviatik B.II

The Aviatik B.II was a two-seat biplane of conventional configuration that also seated its pilot and observer in tandem, open cockpits. Compared to its predecessor, the B.I, the B.II had a more powerful Mercedes D.II engine (120 hp) and revised nose design that faired the powerplant in more neatly, and a single "rhino horn" collector stack for the exhaust. A variety of two- and three-bay wing designs were utilised during production. While originally no armament was fitted (in common with other B- class aircraft), later production versions received a machine gun for the observer. All were withdrawn from front line service by early 1916, however the type continued in use as a trainer for a time with advanced flying training units (it is known that the B.II served in this role at FEA 9 at Darmstadt during 1916).

Austro-Hungarian built D.IIs featured revised, enlarged ailerons, and Austro-Daimler engines.

Aviatik B.III

The B.III was also a reconnaissance aircraft. Aviatik's Austro-Hungarian subsidiary had built the German-designed B.II, and now further developed this design by adding a more powerful engine and armament in the form of a defensive machine gun and bomb racks. It was otherwise similar to Austro-Hungarian built B.IIs, incorporating the revisions that had been made locally to the original design. All were obsolete and out of service by the end of 1916.

Operators

  • Austria-Hungary : KuKLFT.
  • Germany : Luftstreitkrafte.
  • Kingdom of Italy : Corpo Aeronautico Militare.
  • Paraguay.
  • Turkey : Turkish Air Force - Postwar, SAML Aviatik B.I.

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Aviatik B.I of Wikipedia ( authors )

Specifications (B.I)

  • Crew : 2.
  • Wingspan : 13.97 m (45 ft 10 in).
  • Height : 3.3 m (10 ft 10 in).
  • Length : 7.97 m (26 ft 2 in).
  • Gross weight : 1,088 kg (2,399 lb).
  • Maximum speed : 100 km/h (62 mph; 54 kts).
  • Endurance : 4hrs.
  • Service ceiling : 5,000 m (16,404 ft).
  • Powerplant : One Mercedes D.I 6-cylinder liquid-cooled inline engine.
  • Power : 74.5 kW (99.9 hp).
  • Armament : None.

— — — = = — — —

This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Aviatik B.I of Wikipedia ( authors )
Aviatik B.I - B.II - B.III : Your comments on this subject
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