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Bristol Braemar

Military Aircraft

The Bristol Braemar was a large British heavy bomber triplane designed at the end of the First World War for the Royal Air Force, of which only two prototypes were built. It was conceived after the Independent Air Force was established in October 1917, as a machine able to bomb Berlin if required, and it could stow up to six 250 lb bombs internally. The first design placed all four engines in a central engine room and drove the propellers through shafts, but that arrangement was dropped and both completed aircraft carried their engines in tandem pairs, with pusher and tractor propellers. Bristol and Colonial received a contract for three prototypes on 26 February 1918. The first aircraft flew on 13 August 1918 with four 230 hp Siddeley Puma engines; test pilots complained about the view from the cockpit and the controls, so the improved Mk.II was fitted with four 400 hp Liberty L-12 engines. The Braemar never entered RAF service. The third airframe was completed as the Pullman civil transport, and the central engine room idea resurfaced in the proposed steam-powered Tramp.

Facts
Year
1918 1
Engine Class
Piston 1
Status
Prototype 1
Mass (kg)
4831 1
Maximum Mass (kg)
7484 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Bristol Braemar (Wikipedia)

Of Make

Source Bristol Braemar (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Bristol Braemar (Wikipedia)Development, manufacturer
Quote, Development, manufacturer
A contract from the Air Board for three prototypes was awarded to Bristol & Colonial on 26 February 1918.

Originated In

Also in Geography Atlas: where this subject originated.

Source Bristol Braemar (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
The Bristol Braemar was a British heavy bomber aircraft
Sources
1. Bristol Braemar (Wikipedia)
  • Development
    The first prototype Braemar flew on 13 August 1918
  • Specifications
    4 × Liberty L-12 V-12 water-cooled piston engines
  • Specifications, mass
    Empty weight: 10,650 lb (4,831 kg)
  • Specifications, maximum mass
    Gross weight: 16,500 lb (7,484 kg)
  • Lead
    The Bristol Braemar was a British heavy bomber aircraft developed at the end of the First World War for the Royal Air Force.
  • Lead, status
    Only two prototypes were constructed.
  • Development, manufacturer
    A contract from the Air Board for three prototypes was awarded to Bristol & Colonial on 26 February 1918.
  • Lead, country of origin
    The Bristol Braemar was a British heavy bomber aircraft
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