Mitsubishi Kinsei

Kinsei
Type	Radial engine
National origin	Japan
Manufacturer	Mitsubishi Heavy Industries
First run	1932
Major applications	Aichi D3A; Yokosuka D4Y3-D4Y4; Kawasaki Ki-100
Number built	12,228
Developed from	Pratt & Whitney R-1690 Hornet
Developed into	Mitsubishi Shinten, Mitsubishi Zuisei, Mitsubishi Kasei, Ha-43(Ha-211)

The Mitsubishi Kinsei (金星, Venus) was a 14-cylinder, air-cooled, twin-row radial aircraft engine developed by Mitsubishi Heavy Industries in Japan in 1934 for the Imperial Japanese Navy. The Mitsubishi model designation for this engine was A8 while it was an experimental project; in service, it was known as the MK8 "Kinsei" by the Navy. In 1941 the engine was adopted by Army, receiving designation Ha-112^[1] (later Ha-112-I, 1,300hp Army Type 1). In May 1943 it received Ha-33 unified designation code.^[2]

Design and development

Early Kinsei models (1 and 2) had A4 internal designation and their cylinder and detail design was based on the single-row, 9-cylinder air-cooled Pratt and Whitney R-1690 Hornet.^[3]

In 1933 engine underwent a major redesign and redesignated A8. Head layout was reversed to allow exhaust exit to the rear, reducing back-pressure and allowing for a cleaner installation. Compression ratio increased from 5.3:1 to 6.0:1. These changes resulted in a significant performance uplift, compared to previous variants.^[4]

Kinsei 41 saw ever further increase in compression ratio from 6.0:1 to 6.6:1, and a larger supercharger. It's also the first variant to receive a two-digit model numbers. 40 series remained in production from 1936 till the end of the war.

Kinsei 50 series saw the final compression ratio increase to 7.0:1. Indirect fuel injection was fitted as well as a larger two-speed supercharger.

Kinsei 60 series was introduction of direct injection and later, a turbo-supercharger. Its development was run parallel to 50 series. Production started in 1940 and lasted till the end of the war.^[5]

Variants

Early (A4) variants

Data from Goodwin^[6]

Kinsei 1: 820 hp (610 kW) at 2300 rpm at takeoff; 650 hp (480 kW) at 2100 rpm at sea level
Kinsei 2: 830 hp (620 kW) at 2350 rpm at takeoff; 630 hp (470 kW) at 2100 rpm at 1,000 m (3,300 ft)

Late (A8) variants

Data from Goodwin^[7]

Kinsei 3: 790 hp (590 kW) at 2150 rpm at 2,000 m (6,600 ft)
Kinsei 41: 1,075 hp (802 kW) at 2500 rpm at 2,000 m (6,600 ft); 990 hp (740 kW) at 2500 rpm at 2,800 m (9,200 ft); Higher compression ratio, supercharger
Kinsei 42: 1,075 hp (802 kW) at 2500 rpm at 2,000 m (6,600 ft); 990 hp (740 kW) at 2500 rpm at 2,800 m (9,200 ft); Air pump
Kinsei 43: 1,000 hp (750 kW) at 2400 rpm at sea level; 990 hp (740 kW) at 2400 rpm at 2,800 m (9,200 ft); De-rated for economy
Model 44: 1,070 hp (800 kW) at sea level; 1,080 hp (810 kW) at 2,000 m (6,600 ft); Machine gun synchroniser
Kinsei 45: 1,075 hp (802 kW) at sea level; 1,000 hp (750 kW) at 4,180 m (13,710 ft)
Kinsei 46: 930 hp (690 kW) at sea level; 1,070 hp (800 kW) at 4,200 m (13,800 ft); De-rated for extreme economy
Kinsei 51 (MK8A): 1,200 hp (890 kW) at 2500 rpm at 3,000 m (9,800 ft); 1,100 hp (820 kW) at 2500 rpm at 6,200 m (20,300 ft); Redesigned cylinder head, added indirect fuel injection, larger two-speed supercharger
Kinsei 52 (MK8B) (Ha-112-I): 1,200 hp (890 kW) at 2500 rpm at 3,000 m (9,800 ft); 1,100 hp (820 kW) at 2500 rpm at 6,200 m (20,300 ft); Added water injection
Kinsei 53 (MK8C): 1,200 hp (890 kW) at 2500 rpm at 3,000 m (9,800 ft); 1,100 hp (820 kW) at 2500 rpm at 6,200 m (20,300 ft); Higher pressure oil pump
Kinsei 54 (MK8D): 1,200 hp (890 kW) at 2500 rpm at 3,000 m (9,800 ft); 1,100 hp (820 kW) at 2500 rpm at 6,200 m (20,300 ft); Added machine gun synchroniser
Model 61 (Ha-112-II): 1,350 hp (1,010 kW) at 2,000 m (6,600 ft); 1,250 hp (930 kW) at 5,800 m (19,000 ft); Added direct fuel injection
Kinsei 62 (MK8P): 1,350 hp (1,010 kW) at 2600 rpm at 2,000 m (6,600 ft); 1,250 hp (930 kW) at 2600 rpm at 5,800 m (19,000 ft)
Kinsei 62 Ru (Ha-112-II Ru): 1,350 hp (1,010 kW) at 2600 rpm at 2,000 m (6,600 ft); 1,370 hp (1,020 kW) at 2600 rpm at 7,700 m (25,300 ft); 1,240 hp (920 kW) at 2600 rpm at 11,000 m (36,000 ft); Ru-102 turbo-supercharger

Applications

Specifications (Kinsei-44)

Data from Jane's.^[8]

General characteristics

Type: 14-cylinder air-cooled twin-row radial engine
Bore: 140 mm (5.5 in)
Stroke: 150 mm (5.9 in)
Displacement: 32.3 L (1,970 cu in)
Length: 1,646 mm (64.8 in)
Diameter: 1,218 mm (48.0 in)
Dry weight: 545 kg (1,202 lb)

Components

Valvetrain: Overhead valve, one inlet and one exhaust valve per cylinder, pushrod operated.
Supercharger: Centrifugal, single speed.
Oil system: Triple section pump, one pressure pump, two scavenge pumps.
Cooling system: Air-cooled
Reduction gear: Planetary gear, 0.7:1 ratio.

Performance

Power output: 1,075 hp (802 kW) at 2,500 rpm at 2,000 m (6,560 ft) maximum.
Specific power: 24.8 kW/L (0.56 hp/cu in)
Compression ratio: 6.6:1
Power-to-weight ratio: 1.5 kW/kg (0.9 hp/lb)

References

^ Gunston, Bill (1989). World Encyclopaedia of Aero Engines. Cambridge, England: Patrick Stephens Limited. p. 104. ISBN 1-85260-163-9.
^ Goodwin 2017, p. 101.
^ Peattie, Mark R. (2001). Sunburst: The Rise of Japanese Naval Air Power, 1909-1941. Annapolis, Maryland: Naval Institute Press. p. 308. ISBN 1-55750-432-6.
^ Goodwin 2017, p. 90.
^ Goodwin 2017, p. 103.
^ Goodwin 2017, p. 89.
^ Goodwin 2017, p. 119-121.
^ Gunston, Bill (1989). Jane's Fighting Aircraft of World War II. London: Studio Editions Ltd. p. 298. ISBN 0-517-67964-7.

Goodwin, Mike (2017). Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks. ISBN 978-83-65281-32-6.{{cite book}}: CS1 maint: date and year (link)

Bibliography

Goodwin, Mike & Starkings, Peter (2017). Japanese Aero-Engines 1910-1945. Sandomierz, Poland: MMPBooks. ISBN 978-83-65281-32-6.
Matsuoka Hisamitsu, Nakanishi Masayoshi. The History of Mitsubishi Aero Engines 1915–1945. Miki Press, Japan, 2005. ISBN 4-89522-461-9
Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
Jane's Fighting Aircraft of World War II. London. Studio Editions Ltd, 1989. ISBN 0-517-67964-7
Peattie, Mark R., Sunburst: The Rise of Japanese Naval Air Power 1909-1941, Annapolis, Maryland: Naval Institute Press, 2001, ISBN 1-55750-432-6

[1] Gunston, Bill (1989). World Encyclopaedia of Aero Engines. Cambridge, England: Patrick Stephens Limited. p. 104. ISBN 1-85260-163-9.

[FOOTNOTEGoodwin2017101-2] Goodwin 2017, p. 101.

[3] Peattie, Mark R. (2001). Sunburst: The Rise of Japanese Naval Air Power, 1909-1941. Annapolis, Maryland: Naval Institute Press. p. 308. ISBN 1-55750-432-6.

[FOOTNOTEGoodwin201790-4] Goodwin 2017, p. 90.

[FOOTNOTEGoodwin2017103-5] Goodwin 2017, p. 103.

[FOOTNOTEGoodwin201789-6] Goodwin 2017, p. 89.

[FOOTNOTEGoodwin2017119-121-7] Goodwin 2017, p. 119-121.

[8] Gunston, Bill (1989). Jane's Fighting Aircraft of World War II. London: Studio Editions Ltd. p. 298. ISBN 0-517-67964-7.

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v t e Mitsubishi aircraft engines
Piston engines	Ha-42 Ha-43 Kasei Kinsei Shinten Zuisei
Turboshafts	TS1/MG5

v t e Imperial Japanese Army Air Service aero engine designations
1-50	Ha-1 Ha-5 Ha-6 Ha-9 Ha-25 Ha-26 Ha-35 Ha-40 Ha-44 Ha-45
51-100	Ha-60 Ha-70
101-200	Ha-101 Ha-102 Ha-103 Ha-104 Ha-105 Ha-112 Ha-115 Ha-140
200-	Ha-201 Ha-211 Ha-214 Ha-217 Ha-505

v t e Imperial Japanese Navy aero engines
Aichi	Atsuta
Hiro Naval Arsenal	Type 91 Type 94
Mitsubishi	Kasei Kinsei MK9 Shinten Zuisei
Nakajima	Hikari Homare Kotobuki Mamoru Sakae
Tokyo Gasu Denki	Amakaze Kamikaze