M75 armored personnel carrier

M75

An M75 APC at the Brussels army museum.
Type Armored personnel carrier
Place of origin  United States
Service history
In service 1952[1]-late 1950s
Used by  United States,  Belgium
Wars Korean War [2]
Production history
Manufacturer International Harvester Corporation
Number built 1,729
Specifications
Weight 42,000 lb (18,800 kg) [3]
Length 204.5 inches (5.2 m)[3][1]
Width 112 inches (2.5 m)[3][1]
Height 108.5 inches (2.8 m)[3][1]

Main
armament
M2 Browning machine gun
Engine Continental AO-895-4 6-cylinder air-cooled gasoline
295 horsepower (220 kW) (at 2,660 rpm)[3]
Suspension Torsion bar
Fuel capacity 150 US gallons (568 L)[3]
Operational
range
115 miles (185 km)[3]
Speed 43 mph (69 km/h)[3]

The M75 is a American armored personnel carrier that was produced between December 1952 and February 1954, and saw service in the Korean War. It was replaced in U.S. service by the smaller, cheaper, amphibious M59. The M75s were given as military aid to Belgium where they were used until the early 1980s. 1,729 M75s were built before production was halted.

Contents

Development

Towards the end of World War II a tracked, fully enclosed armored personnel carrier was developed under the designation M44 (T16) based on the M18 tank destroyer. The M44 was extremely large (51,000 lb combat weight), carrying 24 infantry as well as a driver, bow gunner and vehicle commander. It was evaluated at Fort Knox and Aberdeen Proving Ground after the end of the war but ultimately the army rejected the M44 as being too large, at the time their tactical doctrine required infantry squads of ten men. As a result only a handful of M44s were built, seeing service in a number of auxiliary roles.

On 21 September 1945 a set of requirements were laid down for a squad sized armored personnel carrier, based on the chassis of the T43 cargo carrier. On 26 September 1946 the development of the armored utility vehicle T18 was approved with the International Harvester Corporation (IHC) contracted to produce four prototypes.

The original mockup featured two remote controlled .50 caliber machine guns, that could be aimed remotely by either the commander or either of two gunners, having a total crew of 14.

The first prototype T18 dropped one the assistant driver but retained the remote controlled machine guns. The T18E1 pilot was unarmed and had a high cupola for the commander, this is sometimes referred to a pilot number 4. The T18E2 replaced the commanders cupola with a T122 machine gun mount that could be fitted with a .30 or .50 caliber machine gun.

Though the original T18E1 prototype was unarmed, the high cupola was replaced with a variety of machine gun mounts, before the M13 cupola with a .50 caliber machine gun was evaluated.

The prototypes were originally powered by a six-cylinder Continental AO-895-2 air-cooled gasoline engine, which exhausted through the hull side grills. This was later replaced with the AO-895-4 in the T18E1,[3] which exhausted through a pipe mounted horizontally across the front of the vehicle.

After acceptance testing the T18E1 was ordered into production in 1952 as the M75. Although the vehicle was developed by IHC, an order for 1,000 were placed with IHC and for 730 at the Food Machinery and Chemical Corporation. Numerous changes were made during the production run to reduce cost and complexity. The number of shock absorbers was halved from four per side to two, and an auxiliary generator/heater was deleted. The two 75 gallon rubber fuel tanks were replaced by a single 150 gallon metal one.

The M75 shared many chassis/suspension components with the M41 light tank, also powered by a Continental air-cooled engine. It had a cross-drive transmission (permitting pivoting, etc.) but was steered through two vertical handles, simulating the laterals of earlier vehicles controlled by track clutching/breaking.

The approximate cost of the vehicle was $72,000 which contributed to the early halting of production. The high profile (height) of the vehicle was also a negative factor. Additionally the engine air cooling vents were considered to be vulnerable to small arms fire. However, the reliability of its drive system was far superior to that of its replacement, the M59.

Description

The M75 has a welded steel hull, which varies in thickness from 1 inch (2.5 cm) to 1.5 inches (3.8 cm) with a line of sight thickness on the front hull of between 1.6 inches (4 cm) and 2 inches (5 cm). Fully loaded, the vehicle weighed approximately 42,000 pounds (19,051 kg).

The M75 has an almost identical layout to later U.S. armored personnel carriers: the driver sits in the front left of the hull, with the air-cooled six-cylinder horizontally opposed Continental AO-895-4 gasoline engine to his right. The driver is provided with an M19 infra-red night vision periscope in later models and four M17 periscopes. Behind the driver and engine in the center of the vehicle sits the commander who is provided with six vision blocks around his hatch. The commander has a cupola which was normally fitted with an M2 machine gun, for which 1,800 rounds were carried in the vehicle. with the infantry behind him in a large compartment. Additionally an M20 Super Bazooka was carried along with 10 rockets, and 180 rounds of ammunition for an M1 or M2 carbine.[3]

The engine developed a maximum of around 295 horsepower (220 kW) at 2,660 rpm, giving the vehicle a top speed of 43 mph (69 km/h). The vehicle carried 150 US gallons (568 L) of gasoline, giving it a road range of around 115 miles (185 km). It has five road wheels and three return rollers on each side.

See also

G-numbers (G260)

Specifications

References

  1. ^ a b c d "Armored Infantry Vehicle M75, late production1-4". AFV database.com. http://afvdb.50megs.com/usa/aivm75.html. Retrieved 2011-03-29. 
  2. ^ "M-75 Armored Personnel Carrier (APC)". Olive-drab.com. http://www.olive-drab.com/idphoto/id_photos_m75apc.php. Retrieved 2011-03-29. 
  3. ^ a b c d e f g h i j k l m n Department of the Army and the Air Force. Military Vehicles (Ordinance Corps Responsibility). Department of the Army Technical Manual, 1953, February 1953 p. 282.

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