- Source: Bristol Jupiter
The Bristol Jupiter is a British nine-cylinder single-row piston radial engine that was built by the Bristol Aeroplane Company. Originally designed late in World War I and known as the Cosmos Jupiter, a lengthy series of upgrades and developments turned it into one of the finest engines of its era.
The Jupiter was widely used on many aircraft designs during the 1920s and 1930s. Thousands of Jupiters of all versions were produced, both by Bristol and abroad under licence.
A turbo-supercharged version of the Jupiter known as the Orion suffered development problems and only a small number were produced. The "Orion" name was later re-used by Bristol for an unrelated turboprop engine.
The Bristol Jupiter was licensed by the Soviet Union as the Shvetsov M-22.
Design and development
The Jupiter was designed during World War I by Roy Fedden of Brazil Straker and later Cosmos Engineering. The first Jupiter was completed by Brazil Straker in 1918 and featured three carburettors, each one feeding three of the engine's nine cylinders via a spiral deflector housed inside the induction chamber. During the rapid downscaling of military spending after the war, Cosmos Engineering became bankrupt in 1920, and was eventually purchased by the Bristol Aeroplane Company on the strengths of the Jupiter design and the encouragement of the Air Ministry. The engine matured into one of the most reliable on the market. It was the first air-cooled engine to pass the Air Ministry full-throttle test, the first to be equipped with automatic boost control, and the first to be fitted to airliners.
The Jupiter was fairly standard in design, but featured four valves per cylinder, which was uncommon at the time. The cylinders were machined from steel forgings, and the cast cylinder heads were later replaced with aluminium alloy following studies by the Royal Aircraft Establishment. In 1927, a change was made to move to a forged head design due to the rejection rate of the castings. The Jupiter VII introduced a mechanically-driven supercharger to the design, and the Jupiter VIII was the first to be fitted with reduction gears.
In 1925, Fedden started designing a replacement for the Jupiter. Using a shorter stroke to increase the revolutions per minute (rpm), and including a supercharger for added power, resulted in the Bristol Mercury of 1927. Applying the same techniques to the original Jupiter-sized engine in 1927 resulted in the Bristol Pegasus. Neither engine would fully replace the Jupiter for a few years.
In 1926 a Jupiter-engined Bristol Bloodhound with the registration G-EBGG completed an endurance flight of 25,074 miles (40,353 kilometres), during which the Jupiter ran for a total of 225 hours and 54 minutes without part failure or replacement.
= Licensed production
=The Jupiter saw widespread use in licensed versions, with fourteen countries eventually producing the engine. In France, Gnome-Rhone produced a version known as the Gnome-Rhône 9 Jupiter that was used in several local civilian designs, as well as achieving some export success. Siemens-Halske took out a licence in Germany and produced several versions of increasing power, eventually resulting in the Bramo 323 Fafnir, which saw use in German wartime aircraft.
In Japan, the Jupiter was licence-built from 1924 by Nakajima, forming the basis of its own subsequent radial aero-engine design, the Nakajima Ha-1 Kotobuki. It was produced in Poland as the PZL Bristol Jupiter, in Italy as the Alfa Romeo 126-RC35, and in Czechoslovakia by Walter Engines. The most produced version was in the Soviet Union, where its Shvetsov M-22 version powered the initial Type 4 version of the Polikarpov I-16 (55 units produced). Type 4 Polikarpovs can be identified by their lack of exhaust stubs, rounded NACA cowling and lack of cowling shutters, features which were introduced on the Shvetsov M-25 powered Type 5 and later variants (total production 4,500+ units). Production started in 1918 and ceased in 1930.
Variants
The Jupiter was produced in many variants, one of which was the Bristol Orion of 1926. Metallurgy problems with this turbo-supercharged engine caused the project to be abandoned after only nine engines had been built.
Brazil Straker (Cosmos) Jupiter I
(1918) 400 hp (300 kW); only two engines assembled.
Cosmos Jupiter II
(1918) 400 hp (300 kW); a single engine assembled.
Bristol Jupiter II
(1923) 400 hp (300 kW).
Bristol Jupiter III
(1923) 400 hp (300 kW).
Bristol Jupiter IV
(1926) 430 hp (320 kW); fitted with variable valve timing and a Bristol Triplex carburettor.
Bristol Jupiter V
(1925) 480 hp (360 kW).
Bristol Jupiter VI
(1927) 520 hp (390 kW); produced in both high- (6.3:1) and low- (5.3:1) compression ratio versions.
Bristol Jupiter VIA
(1927) 440 hp (330 kW); civil version of Jupiter VI.
Bristol Jupiter VIFH
(1932) 440 hp (330 kW); version of Jupiter VI equipped with gas starter motor.
Bristol Jupiter VIFL
(1932) 440 hp (330 kW); version of Jupiter VI with compression ratio of 5.15:1.
Bristol Jupiter VIFM
(1932) 440 hp (330 kW); version of Jupiter VI with compression ratio of 5.3:1.
Bristol Jupiter VIFS
(1932) 400 hp (300 kW); version of Jupiter VI with compression ratio of 6.3:1.
Bristol Jupiter VII
(1928) 375 hp (280 kW); fitted with supercharger, with compression ratio of 5.3:1; also manufactured by Gnome-Rhone as the 9ASB.
Bristol Jupiter VIIF
(1929) 480 hp (360 kW); version of Jupiter VII with forged cylinder heads.
Bristol Jupiter VIIFP
(1930) 480 hp (360 kW); version of Jupiter VII with pressure feed lubrication to wrist-pins.
Bristol Jupiter VIII
(1929) 440 hp (330 kW); first version with propeller reduction gearing; compression ratio 6.3:1.
Bristol Jupiter VIIIF
(1929) 460 hp (340 kW); version of Jupiter VIII with forged cylinder heads and lowered compression ratio (5.8:1).
Bristol Jupiter VIIIFP
(1929) 460 hp (340 kW); version of Jupiter VIII with pressure feed lubrication (time between overhauls at this stage in development was only 150 hours due to multiple failures).
Bristol Jupiter IX
480 hp (360 kW); compression ratio 5.3:1.
Bristol Jupiter IXF
550 hp (410 kW); version of Jupiter IX with forged cylinder heads
Bristol Jupiter X
470 hp (350 kW); compression ratio 5.3:1.
Bristol Jupiter XF
540 hp (400 kW); version of Jupiter X with forged cylinder heads
Bristol Jupiter XFA
483 hp (360 kW)
Bristol Jupiter XFAM
580 hp (430 kW)
Bristol Jupiter XFBM
580 hp (430 kW)
Bristol Jupiter XFS
Fully supercharged.
Bristol Jupiter XI
Compression ratio 5.15:1.
Bristol Jupiter XIF
500 hp (370 kW); compression ratio 5.15:1.
Bristol Jupiter XIFA
480 hp (360 kW); version of Jupiter XIF with 0.656:1 propeller gear reduction ratio
Bristol Jupiter XIFP
525 hp (391 kW); version of Jupiter XIF with pressure feed lubrication.
Bristol Orion I
(1926) Jupiter III, turbo-supercharged, abandoned programme.
Gnome-Rhône 9A Jupiter
French licence production primarily of 9A, 9Aa, 9Ab, 9Ac, 9Akx and 9Ad variants.
Siemens-Halske Sh20, Sh21 and Sh22
Siemens-Halske took out a licence in Germany and produced several versions of increasing power, eventually resulting in the Bramo 323 Fafnir, which saw use in wartime models.
Nakajima Ha-1 Kotobuki
In Japan, the Jupiter was licence-built from 1924 by Nakajima.
PZL Bristol Jupiter
Polish production.
Alfa Romeo Jupiter
Italian licence production, 420 hp (310 kW).
Alfa 126 R.C.35
Alfa Romeo developed variant
Walter Jupiter
Licence production in Czechoslovakia by Walter Engines
Shvetsov M-22
The most produced version; manufactured in the Soviet Union.
IAM 9AD Jupiter
Licence production of the Gnome-Rhône 9A in Yugoslavia
SABCA Jupiter
licensed production in Belgium by SABCA (Société Anonyme Belge de Constructions Aéronautiques)
Piaggio-Jupiter
Licensed production by Piaggio
Applications
The Jupiter is probably best known for powering the Handley Page H.P.42 airliners, which flew the London-Paris route in the 1930s. Other civilian uses included the de Havilland Giant Moth and de Havilland Hercules, the Junkers G 31 and the huge Dornier Do X flying boat, which used no less than twelve engines.
Military uses were less common, but included the parent company's Bristol Bulldog, as well as the Gloster Gamecock and Boulton Paul Sidestrand. It was also found in prototypes around the world, from Japan to Sweden.
By 1929 the Bristol Jupiter had flown in 262 different aircraft types, it was noted in the French press at that year's Paris Air Show that the Jupiter and its licence-built versions were powering 80% of the aircraft on display.
Note:
= Cosmos Jupiter
=Bristol Badger
Bristol Bullet
Sopwith Schneider
Westland Limousine
= Bristol Jupiter
== Gnome-Rhône Jupiter
=Bernard SIMB AB 12
Blanchard BB-1
Breguet 19
Fizir F1M-Jupiter
Latécoère 6
Lioré et Olivier LeO H-15
Potez 29/4
Wibault Wib.220
Denhaut Hy.479
= Shvetsov M-22
=Kalinin K-5
Kalinin K-12
Polikarpov I-5
Polikarpov I-15
Polikarpov I-16
Tupolev I-4
Yakovlev AIR-7
Engines on display
A Bristol Jupiter VI is on static display at Aerospace Bristol in the former Bristol Aeroplane Company factory complex in Filton, a suburb of Bristol, United Kingdom.
A Bristol Jupiter VIIF is on static display at the Shuttleworth Collection in Old Warden, United Kingdom.
A Bristol Jupiter VIIIF is on static display at the Steven F. Udvar-Hazy Center of the National Air and Space Museum at Washington Dulles International Airport in Fairfax County, Virginia, United States.
A Bristol Bulldog complete with a Jupiter VIIFP engine is on static display at the Royal Air Force Museum London in Hendon, United Kingdom.
Specifications (Jupiter XFA)
Data from Lumsden
= General characteristics
=Type: Nine-cylinder, naturally aspirated, air-cooled radial engine
Bore: 5.75 in (146 mm)
Stroke: 7.5 in (190 mm)
Displacement: 1,753 in3 (28.7 L)
Diameter: 54.5 in (1,384 mm)
Dry weight: 995 lb (451 kg)
= Components
=Valvetrain: Overhead poppet valve, four valves per cylinder, two intake and two exhaust
Supercharger: Single speed, single stage
Fuel type: 73-77 octane petrol
Cooling system: Air-cooled
= Performance
=Power output: * 550 hp (414 kW) at 2,200 rpm at 11,000 ft (3,350 m) - maximum power limited to five minutes operation.
525 hp (391 kW) at 2,000 rpm - maximum continuous power at 11,000 ft (3,350 m)
483 hp (360 kW) at 2,000 rpm - takeoff power
Specific power: 0.31 hp/in3 (14.4 kW/L)
Compression ratio: 5.3:1
Power-to-weight ratio: 0.55 hp/lb (0.92 kW/kg)
See also
Related development
Alfa Romeo 125
Bristol Mercury
Bristol Pegasus
Nakajima Kotobuki
Siemens-Halske Sh 22
Comparable engines
BMW 132
Pratt & Whitney R-1340, first of the famous Wasp radial engine line
Pratt & Whitney R-1690 Hornet
Wright R-1820 Cyclone 9
Related lists
List of aircraft engines
References
= Bibliography
=Bridgman, L. (ed.) Jane's Fighting Aircraft of World War II. New York: Crescent Books, 1998. ISBN 0-517-67964-7
Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
Gunston, Bill. Development of Piston Aero Engines. Cambridge, England. Patrick Stephens Limited, 2006. ISBN 0-7509-4478-1
Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
Smith, G. Geoffrey, ed. (9 March 1939). "Rise of the Radials". Flight. XXXV (1576): 236–244. Retrieved 17 May 2018.
Further reading
Gunston, Bill. By Jupiter! The Life of Sir Roy Fedden. The Johns Hopkins University Press.
External links
"The Cosmos Aero Engines". Flight. XI (27): 869–871. 3 July 1919. No. 549. Retrieved 12 January 2011. Contemporary article on Cosmos Engineering's air-cooled radial engines. Photos of the Cosmos Jupiter are on page 870, and a short technical description is on page 871.
Bristol Jupiter endurance test - Flight, March 1926
A 1929 Flight advertisement for the Jupiter
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