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A High Speed Racing Monoplane which holds Many Long-Distance Flying Records
The aircraft was a twin-engined low-wing monoplane. Retractable undercarriage units were provided which drew up into the engine nascelles. The engines originally fitted to the Comet were De Havilland Gipsy Six of a specially tuned type. These legitimately may be said to have been the forerunners of the Gipsy Six Series II engines which were fitted in the Comets that made some of the later long-distance flights. Two seats were provided in the fuselage aft of the wings and were fitted with an enclosing cover. Short trailing edge flaps were provided between the fuselage and the engine nascelles. To retract, the wheels moved directly backwards and upwards. The wings of the Comet tapered towards their tips and had a stressed skin covering on a wooden framework. Plywood covering was used for the wings, which had a final layer of fabric. Similarly the fuselage was a wooden frame covered with plywood. The retractable undercarriage units were hand-operated by a screw jack controlled from the cockpit by a continuous cable. Wheel brakes were also provided.
![]() The MacRobertson Trophy, won by the Comet in 1934
The special Gipsy Six engines developed 220 horse-power each at 2,350 revolutions a minute at sea level. The petrol tanks had a total capacity of 255 gallons. This supply was carried in two petrol tanks in the forepart of the fuselage and in a small tank behind the cockpit. Engine oil was carried in the engine nascelles. The engines were fitted with automatically-operated two-position variable-pitch airscrews; the pitch was set fine for take-off using a bicycle pump, then coarsened automatically with air pressure as the aircraft climbed.
The initial difference between the special Gipsy Six engines and the standard Gipsy Six Series I engine was in the increased compression ratio. The span of the mail plane was 44 feet, the overall length of the aircraft 29 feet and the overall height nine feet. The maximum permissible all-up weight of the Comet was 5,550 lb. This included an allowance of 400 lb for the crew and their parachutes.
The maximum speed of the aeroplane with full load was 225 miles an hour at sea level, and the cruising speed about 200 miles an hour at 10,000 feet. At this height and speed the maximum range of the aircraft was 2,950 miles; at full throttle at 10,000 feet, and at a speed of 220 miles an hour the range was 2,550 miles. The initial rate of climb was 1,100 feet a minute and the time taken to climb to 10,000 feet 13 minutes. Both these figures were obtained with the airscrew set to fine pitch.
The take-off run was about 450 yards and the landing run about 350 yards, with a load of 5,000 lb. The ceiling of the Comet was 21,000 feet and the absolute ceiling on one engine 4,000 feet. The normal stalling speed of the aircraft with the flaps in use was 78 miles an hour, but with a light load was reduced to 63 miles an hour.
Back in service
Having been built for, and won, the 1934 MacRobertson Trophy Race, DH88 Comet G-ACSS (Grosvenor House) performed various other tasks before ending up in storage during and after WWII. Eventually it was handed over to The Shuttleworth Collection at Old Warden in Bedfordshire as a static exhibit in 1965.
That could have been the end for this classic machine, parked in a hangar as a walk-round exhibit. However, it was restored to former flying glory helped by grants from the Transport Trust and Hawker Siddeley Aviation (the company which had taken over de Havilland's) and from about fifty organisations in the aviation and allied industries.
Grosvenor House flew again in its original colour scheme for the first time in 49 years on Sunday May 17, 1987, and has since proved to be a popular performer at the Old Warden classic displays. One difference between the original and the rebuild - the 1934 Grosvenor House had a tailskid, which on the 'modern' version has been replaced with a tailwheel.
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