Mitsubishi Saturn engine

The 4G30 displaces 1.3 L (1,289 cc). It is an 8-valve SOHC design with an aluminium head and iron block. The engine has five main bearings. Power was 87 hp (65 kW).

Bore x Stroke: 73 mm × 77 mm (2.87 in × 3.03 in)

The 4G31 displaces 1.5 L (1,499 cc). It is an 8-valve SOHC design with an aluminium head and iron block. The engine has five main bearings. Power was 95–105 hp (71–78 kW) depending on which carburetor combo was used. An updated version with central-point electronic fuel injection was installed in Mirages and Lancers from 1986 on.[1] A version for industrial use has 37 PS (27 kW) at 3000 rpm.[2]

Bore x Stroke: 74.5 mm × 86 mm (2.93 in × 3.39 in)

In 1970, the 4G32 was introduced, and it displaces 1.6 L (1,597 cc). It is an eight-valve SOHC design with an aluminium head and iron block. The engine has five main bearings, a cross flow head and a single down draught carburetor. Firing order is 1-3-4-2. The GSR versions used two twin-barrel Mikuni-built Solex carburetors for a total of 110 hp (82 kW) (SAE).

4G32 ECI engine in a Mitsubishi Mirage

A version with an early iteration of Mitsubishi's MCA lean-burn system (MCA-IIB), fulfilling the intermediate Japanese exhaust regulations for 1975, was called G32A. This was built for less than one year, as the new MCA engine arrived in November 1975. Those with the later, cleaner yet, "MCA-Jet" system were called G32B. Later, the G32B also came in a fuel injected, turbocharged model. For competition, a version of the 4G32 engine was made with a DOHC eight-valve cylinder head, and fitted with two twin-choke 40 mm (1.6 in) Solex sidedraft carburettors.

Bore x Stroke: 77 mm × 86 mm (3.03 in × 3.39 in)

The 4G33 displaces 1.4 L (1,440 cc) from a 73 mm × 86 mm (2.87 in × 3.39 in) bore and stroke. There was also an MCA-Jet equipped G33B developed to fulfill the 1978 Japanese emissions regulations.

The 4G35 displaces 1.7 L (1,686 cc). It is an 8-valve SOHC design with an aluminium head and iron block. The engine has five main bearings. Power was 105–115 hp (78–86 kW) depending on which carburetor combo was used.

Bore x Stroke: 79 mm × 86 mm (3.11 in × 3.39 in)

Applications:

• 1973.01-1973.06 Mitsubishi Galant GS (A55)
• 1972.02-1976 Mitsubishi Galant GTO (A55C)

The 4G36 displaces 1.2 L (1,239 cc). 73 mm × 74 mm (2.87 in × 2.91 in) bore and stroke.

Applications:

• Mitsubishi Celeste
• Mitsubishi Colt
• Mitsubishi Lancer

The 8-valve SOHC 4G37 displaces 1.8 L (1,755 cc).

Bore x Stroke: 80.6 mm × 86 mm (3.17 in × 3.39 in)

Compression Ratio: 9.5:1

Applications:

• Mitsubishi Chariot/Space Wagon 1983–91
• Mitsubishi Cordia
• Mitsubishi Galant
• Mitsubishi Eclipse 1990–1994
• Mitsubishi Lancer/Lancer Fiore/Mirage - 4WD Station wagons only
• Mitsubishi Tredia

By other brands:

• Eagle Talon DL 1993–1994
• Plymouth Laser 1990–1994

The 6G34, referred to by Mitsubishi as the Saturn 6, is a 12-valve SOHC straight-6 of 2.0 L (1,994 cc) displacement.

The 6G34 was used only in the Mitsubishi Debonair Executive from September 1970 to June 1976, and saw very limited production. Effectively, the design was that of the standard Saturn four-cylinder block with two additional cylinders grafted on to replace the KE64.

Applications:

• Mitsubishi Debonair 1970.09-1976.06 (Japan only)

Wikimedia Commons has media related to Mitsubishi 4G3 engines.

• List of Mitsubishi engines
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• "Engine Epic Part 8 - Mitsubishi Engines", Michael Knowling, Autospeed, issue 48, 21 September 1999