Origins During the 1930s, demand for air travel was rapidly growing. The British national flag airline
Imperial Airways sought to fully expand air service across the British Empire. Imperial Airways' technical adviser, planned a specification for a new type of aircraft to serve passenger and freight requirements throughout the world. This required an aircraft to carry 24 passengers in comfort, as well as
airmail or freight while having a
cruising speed of , a normal range of at least and the capability for an extended range of to cross the North
Atlantic. Shorts developed its own machinery to produce the necessary T-shaped
Hiduminium alloy lengths that comprised the main
spar. A specialised and patented
flap, known as
Gouge flaps after its creator, caused only a small increase in drag, while the wing's lift coefficient was increased by 30 percent, the landing speed reduced by 12 per cent, and no
trim changes were needed. Early flights were relatively trouble-free, and Parker was satisfied with its performance and handling. On 17 September 1936, G-ADHL first flew for Imperial Airways, with the final proving flight to
Marseille, France took place on 22 October 1936. The first series of the Short Empires, the
S.23, could carry five crew, 17 passengers, and of cargo at a maximum speed of and was powered by four
Bristol Pegasus Xc
radial engines. The second Empire and the first of the long-range models, registered G-ADHM, named
Caledonia, made its first flight on 15 September 1936 and was delivered to Imperial Airways on 4 December 1936. In late 1937, Imperial Airways placed a follow-on order for another 11 Empires. When combined with the original order of 28, this had the distinction of being the largest order by a single customer placed for a British civil aircraft at that time. While the first three aircraft of the additional order were of the typical S.23 class, intended for Qantas Empire Airways, the rest had a number of detail changes and were designated the
S.30. Short's
Rochester factory produced all 43 Empires built.
Further development The
S.30 series was fitted with four
Bristol Perseus XIIc sleeve valve engines in the place of the Pegasus engines. the Perseus engines were each lighter and 17.3% more fuel efficient, but developed less power. It was roughly 15 percent larger, as well as using the much more powerful
Bristol Hercules radial engine and a further improved hull design. It was intended to be used on the north Atlantic route. ==Design==