Bristol Type 138

Infobox Aircraft
name=Type 138 High Altitude Monoplane


caption=The Type 138A over Farnborough c. 1937
type=High-altitude research aircraft
manufacturer=Bristol Aeroplane Company
designer=Frank Barnwell
first flight=11 May 1936
introduced=
retired=
status=out of service
primary user=Royal Aircraft Establishment
more users=
produced=
number built=1 (+1 Type 138B airframe not completed)
unit cost=
variants with their own articles=The Bristol Type 138 High Altitude Monoplane was a British, high-altitude research aircraft of the 1930s. The Type 138 was a single-engine, low-wing monoplane with a fixed, tailwheel undercarriage.

Design and development

The Type 138 was born of a period of intense competition between aviation manufacturers in the 1920s and 1930s. There was a great deal of prestige, as well as technological progress, to be gained from breaking one of the major aviation records: airspeed, distance and altitude. By the 1930s, absolute speed and distance records had passed beyond the compass of individual companies and required the active collaboration of national governments. As a result, the focus of companies centred on high-altitude development.

Bristol were well placed to move in this field but in the event, they found themselves lagging. Between 1929 and 1934, there were a number of altitude records established by rival machines including a Junkers W.34, a Vickers Vespa and a Caproni biplane, as well as the first flight over Everest by a pair of Westland Wallaces in 1933; all these aircraft used Bristol or Bristol-designed engines. Barnes, C.H. "Bristol Aircraft since 1910". London: Putnam, 1964. ISBN 0-85177-823-2.]

Divining Air Ministry interest from the Everest expedition, Barnwell proposed a purpose-built, high-altitude, research aircraft in November 1933. This Type 138 was a large, single-engine, single-seat monoplane with retractable undercarriage and a highly supercharged Pegasus engine. Nothing come of this until Renato Donati set a new record in April 1934; public opinion demanded a new, government-sponsored record attempt. In June, the Air Ministry issued Specification 2/34 for two prototypes capable of reaching 50,000 ft (15,034 m). Thetford, Owen. "Aircraft of the Royal Air Force 1918-57, 1st edition". London: Putnam, 1957. Barnwell revised the 138 to produce the Type 138A. This was of the original size and configuration but had a special, two-stage supercharged Pegasus and, although remaining basically a single-seater, had provision for an observer's cockpit to be fitted if required. Weight-saving was a priority; the airframe other than the steel tube engine mount was a wooden monocoque and the undercarriage was replaced with a lightweight, fixed assembly.

The supercharger installation, with detail work by Clifford Tinson, was a two-stage system; the first-stage compressor was permanently engaged but the second-stage was engaged by the pilot at the correct height. The system employed an intercooler between first and second stages.

Much research was carried out by the Royal Aircraft Establishment and National Physical Laboratory both to establish the most efficient design for the aircraft and to develop a reliable pressure suit for the pilot. Sir Robert Davis of Siebe Gorman and Professor J.S. Haldane were instrumental in developing the helmet.

The aircraft was complete in early 1936 and was flown for the first time, from Filton on 11 May, piloted by Cyril Uwins, who had flown the Vickers Vespa on its world record flight. Two more flights were made, the pressure helmet was tested at Farnborough and the aircraft was returned to Filton for the special four-blade airscrew to be fitted. On 5 September, the 138A was deemed ready and was flown back to Farnborough.

Operational history

Squadron Leader F.R.D. Swain was selected to pilot the high-altitude flights. On 28 September 1936, Swain took off from Farnborough and climbed to an indicated 51,000 feet, engaging the auxiliary supercharger at 35,000 feet. Swain ran low on oxygen on the two-hour flight and had to break the window of his pressure helmet once he had descended to a safe height. The data from this flight was homologated by the Federation Aeronautique Internationale as a world's record of 49,967 ft (15,230 m).

After this flight, further development of the aircraft resulted in a number of small modifications. In this mildly revised form, the 138A made six further flights to around 50,000 feet. During this period, Italy increased the record to 51,364 ft. In response, on 30 June 1937, Flight Lieutenant M.J. Adam undertook a 2¼-hour flight in which he achieved a record altitude, later homologated at 53,937 feet (16,440 m). Despite the cockpit canopy cracking, Adam was saved from injury by his pressure suit . After this, research flights continued but no further records were attempted.

A second machine was ordered as the Type 138B in 1935. This was to be a two-seater powered by a Rolls-Royce Kestrel S engine fitted with a similar two-stage supercharger installation and generating 500 hp. The airframe was delivered to Farnborough Airfield in 1937 for completion but the engine installation was never completed.

Variants

;Type 138:Not built.

;Type 138A:One built

;Type 138B:One built, engine installation never completed

Operators

;UK
*Royal Air Force

pecifications (138A)

aircraft specifications
plane or copter?= plane
jet or prop?= prop

ref=Bristol Aircraft since 1910
crew=1
capacity=
length main= 44 ft 0 in
length alt= 13.41 m
span main= 66 ft 0 in
span alt= 20.12 m
height main= 10 ft 3 in
height alt= 3.13 m
area main= 568 ft²
area alt= 52.8 m²
airfoil=
empty weight main= 4,391 lb
empty weight alt= 1,996 kg
loaded weight main= 5,310 lb
loaded weight alt= 2,414 kg
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=

engine (prop)=Bristol Pegasus P.E.6S
type of prop=radial
number of props=1
power main= 500 hp
power alt= 373 kW
power original=
max speed main= 107 knots
max speed alt= 123 mph, 198 km/h
cruise speed main=
cruise speed alt=
never exceed speed main=
never exceed speed alt=
stall speed main=
stall speed alt=
range main=
range alt=
ceiling main= 54,000 ft
ceiling alt= 16,500 m
climb rate main= 1,430 ft/min
climb rate alt= 7.27 m/s
climb rate more= at 40,000 ft
loading main= 9.35 lb/ft²
loading alt= 45.7 kg/m²
thrust/weight=
power/mass main= 0.0942 hp/lb
power/mass alt= 0.155 kW/kg
more performance=
*Endurance: 2¼ hours

armament=

avionics=

aircontent

related=

similar aircraft=

see also=

References

External links

* [http://www.unrealaircraft.com/gravity/bristol138.php|Unreal Aircraft]