M22 Locust
The M22 Locust was an American light tank developed during World War II specifically for airborne operations, designed to be transported by glider and provide mobile fire support to paratrooper units with its compact size and light weight of approximately 7.4 tonnes.[1][2] Development of the M22 began in late 1941, initiated by the U.S. Army to meet the need for an air-portable armored vehicle capable of deployment via aircraft like the C-54 Skymaster, following collaboration between the Army Air Force, Armored Force, and Ordnance Department.[1] The design evolved from prototypes designated T9 and T9E1, produced by the Marmon-Herrington Company, with production beginning in April 1943 and the vehicle accepted as the Light Tank M22, classified as limited standard.[2][1][3] Although intended for U.S. airborne divisions, the tank was deemed obsolete by December 1944 due to its thin armor and limited firepower against contemporary threats, leading to no combat deployment by American forces.[2] The M22 featured a three-man crew operating from an open-top turret and hull, with primary armament consisting of a 37 mm M6 low-pressure gun capable of firing 50 rounds, supplemented by a coaxial 7.62 mm (0.30 in) M1919A4 Browning machine gun with 2,500 rounds of ammunition.[1][2] Its armor protection varied from 12 mm to 25 mm in thickness, offering minimal defense against anti-tank weapons or even heavy machine guns, while the vertical volute spring suspension (VVSS) system supported mobility across varied terrain.[1] Powered by a 162 horsepower Lycoming O-435T six-cylinder air-cooled engine, the tank achieved a top road speed of 56 km/h (35 mph) and an operational range of 177 km, with dimensions of 3.94 m in length, 2.25 m in width, and 1.84 m in height (without the open turret).[2][1] Production ran from April 1943 to February 1944, resulting in 830 units manufactured.[1] The British Army received 260 examples under Lend-Lease, redesignating it the Locust and modifying some with a Littlejohn adaptor on the main gun for improved anti-armor performance, before assigning them to the 6th Airborne Armoured Reconnaissance Regiment of the 6th Airborne Division.[2] Its sole major combat action occurred during Operation Varsity on March 24, 1945, when seven Locusts supported the Allied Rhine crossing in Germany, providing reconnaissance and infantry support despite mechanical issues and vulnerability to enemy fire that led to several losses.[1][2] Post-war, surviving units were largely scrapped, though a small number served with the Egyptian Army into the late 1940s.[2]Development
Background and requirements
Prior to the United States' entry into World War II, the U.S. Army had shown growing interest in airborne operations, spurred by observations of German paratrooper tactics in the 1940 invasions of the Low Countries and the rapid development of glider-borne assaults. This vulnerability of lightly armed paratroopers without armored support highlighted the need for lightweight, air-transportable vehicles to provide mobile fire support in rapid deployments behind enemy lines. British experiments with gliders in 1940, including requests for collaborative airborne tank designs through the British Air Commission in early 1941, further influenced U.S. efforts to create specialized equipment for airborne forces despite America's initial neutrality.[1] In response to these needs, the U.S. Army issued specific requirements in May 1941 for an airborne light tank, designated the T9, weighing no more than 7.5 short tons (approximately 6,800 kg) to ensure compatibility with transport aircraft like the Douglas C-54 Skymaster. The design emphasized a compact footprint and low silhouette to facilitate airdrop operations, allowing the tank to be slung beneath the aircraft fuselage with the turret removed for storage inside, thereby minimizing logistical burdens and enabling quick reinforcement of isolated paratrooper units.[4][1] The Infantry Board and Ordnance Department played pivotal roles in defining the T9's purpose, collaborating with the Armored Force and U.S. Army Air Forces to outline a vehicle optimized for infantry support in airborne assaults, prioritizing mobility and ease of air delivery over heavy armor or firepower. This focused on enabling the tank to operate independently until linked up with main forces, without requiring extensive supply lines. As a direct response to these specifications, the tank incorporated a 37 mm main gun for adequate anti-infantry and light vehicle engagement.[1][5] In July 1941, the Ordnance Department awarded an initial contract to the Marmon-Herrington Company to develop the T9 prototype, leveraging the firm's prior experience with lightweight tank designs such as the CTL series for export. This selection followed evaluations of proposals from other manufacturers, emphasizing cost-effectiveness and rapid prototyping to meet the urgent demands of expanding airborne capabilities.[4][6]Design and production
The design of the M22 Locust originated with the T9 prototype, developed by Marmon-Herrington starting in late 1941, following a U.S. Army contract awarded in July 1941 and influenced by British requests.[1] This initial version featured a basic riveted hull and mechanical turret traverse, but subsequent iterations addressed production and transport needs.[1] The refined T9E1 variant, also completed in 1942, introduced key engineering enhancements including a welded hull for improved structural integrity, rubber-block tracks to enhance traction and reduce noise, and a hydraulic turret traverse mechanism for smoother operation.[1] Central to the design was the turret's quick-release mounting system, allowing removal in under 10 minutes to fit within aircraft cargo limits, alongside compact dimensions of 3.94 m in length, 2.25 m in width, and 1.84 m in height.[1] An initial development contract was awarded in 1941, with pilot models tested in 1942; full production began in April 1943, with 830 units manufactured by Marmon-Herrington until February 1944. Of these, 260 were supplied to Britain via Lend-Lease for airborne use, incorporating features like the British No. 19 radio set for standardized communications.[1]Testing and evaluation
The U.S. Army initiated testing of the T9E1 prototypes, precursors to the M22 Locust, at Aberdeen Proving Ground in December 1942, with evaluations continuing into 1943 to assess durability, reliability, and overall performance.[1] These trials included airdrop simulations, where the vehicle demonstrated compatibility with the C-54 Skymaster aircraft for parachute deployment when the turret was removed. In February 1943, the prototypes were transferred to the Armored Force for further field assessments, revealing issues with the transmission and powertrain.[1] Mobility evaluations during these tests highlighted the vehicle's capabilities on varied terrains, achieving a top speed of 64 km/h (40 mph) on roads due to its 162 hp Lycoming O-435 engine and lightweight 7.5-ton design.[7] It successfully climbed gradients up to 50% and crossed trenches 1.68 m wide, but performance faltered on steeper slopes exceeding 30 degrees and rough off-road conditions, attributed to a suboptimal power-to-weight ratio that limited acceleration and hill-climbing under load.[1] Several mechanical shortcomings were identified, including unreliable engine cooling that led to overheating during extended operations, frequent track shedding on uneven ground, and constrained internal space resulting in only 50 rounds of ammunition storage for the 37 mm M6 gun.[1] A September 1943 preliminary report from the U.S. Army Armored Board at Fort Knox deemed the T9E1 unsatisfactory overall, citing inadequate reliability, armor protection, and combat effectiveness, though it acknowledged potential for airborne roles with modifications.[1] British evaluations of the second T9E1 prototype began in late 1942 upon its shipment to England, with more extensive trials in 1943–1944 focusing on integration with the General Aircraft GAL.49 Hamilcar glider and operational suitability.[1] These tests confirmed similar faults in mechanical reliability but prompted minor modifications, such as improved periscopes for better visibility and a Littlejohn adaptor for the main gun to enhance penetration.[1] Despite persistent flaws, the British accepted the design in 1944 for urgent airborne requirements, designating it the Locust and prioritizing production for reconnaissance units.[1]Design characteristics
Chassis and mobility
The M22 Locust employed a welded chassis constructed from rolled homogeneous steel plates, forming a compact hull that accommodated a crew of three: the driver positioned in the forward left hull, the gunner on the left side of the turret, and the commander serving as loader on the right side of the turret. This internal layout optimized space in the confined 12-foot-11-inch-long vehicle, with the driver's compartment featuring a sloped front glacis plate that enhanced ergonomics by providing deflection angles while maintaining visibility through periscopes and vision ports.[3] The suspension system consisted of a vertical volute spring setup (VVSS) with four small road wheels per side arranged in two bogies, supplemented by two return rollers, a 22-tooth front drive sprocket, and a trailing adjustable idler with volute springs. This configuration supported the tank's 7.5-ton combat weight while ensuring stability and ease of maintenance during airborne operations.[3] Power was supplied by a rear-mounted Lycoming O-435T six-cylinder horizontally opposed air-cooled gasoline engine, producing 162 net horsepower at 2,800 rpm (with a gross output of 192 hp). The engine drove a four-speed manual transmission and controlled differential steering, with a fuel capacity of 57 US gallons enabling a road range of about 110 miles at a top speed of 35 mph.[3] Mobility characteristics included a low ground pressure of 7.1 psi for effective cross-country performance, a fording depth of 36 inches, a vertical obstacle climb of 18 inches, and a trench-crossing capability of 66 inches. The chassis design facilitated rapid disassembly into major components for air transport via glider or aircraft, with production models incorporating transport adaptations such as removable transmission assemblies to expedite loading.[3]Armament and protection
The M22 Locust was equipped with a primary armament of a 37 mm Gun M6 mounted in the M53 mount within a small, open-top turret. This gun, weighing 84 kg and measuring 2.1 m in length, was capable of firing a variety of ammunition types, including armor-piercing (AP M74), armor-piercing capped (APC M51), high-explosive (HE M63), and canister (M2) rounds, with a total capacity of 50 projectiles stored in the turret and hull. The weapon had a maximum range of approximately 6.9 km (4.3 mi), though effective direct fire range was limited to about 1-2 km, a muzzle velocity of around 884 m/s for AP projectiles, and a rate of fire up to 30 rounds per minute.[3][1][8] A coaxial 7.62 mm (0.30 in) Browning M1919A4 machine gun provided secondary armament, with 2,500 rounds of ammunition carried aboard, primarily for anti-infantry suppression. The turret was traversed manually via a hand-operated mechanism, allowing a full 360° rotation, with a maximum traverse time of 15 seconds for a complete circle; elevation ranged from -10° to +30°. The gunner utilized an M46 or M46A2 telescope integrated into an M8 or M8A1 periscope for aiming, while the commander relied on a periscope sight for observation and target acquisition. These features prioritized simplicity and low weight over powered traversal systems, reflecting the tank's airborne design constraints.[3][9] The Locust's armor was constructed from rolled homogeneous steel for the hull and cast homogeneous steel for the turret, welded together to form a lightweight protective envelope that sacrificed thickness for air-transportability. Maximum armor thickness reached 25.4 mm (1 in) on critical areas such as the turret front (sloped at 30°), gun shield (50° slope), driver's head cover, and lower hull front, while hull sides measured 9.5-12.7 mm (0.375-0.5 in) with slopes of 45° on upper sides. The turret sides and rear were also 25.4 mm, but the overall configuration left the vehicle highly vulnerable to anti-tank weapons, including German 37 mm Pak 36 guns, which could penetrate its armor at ranges beyond 200 yards. Thinner roof (9.5-19.1 mm) and floor (12.7 mm) plating offered minimal protection against top-attack or indirect fire.[3][1]| Component | Thickness | Slope |
|---|---|---|
| Hull Upper Front | 12.7 mm | 65° |
| Hull Lower Front | 25.4 mm | 0° |
| Hull Upper Sides | 9.5 mm | 45° |
| Hull Lower Sides | 12.7 mm | 0° |
| Hull Rear | 12.7 mm | 9° |
| Hull Top/Floor | 9.5-12.7 mm | 90° |
| Turret Front | 25.4 mm | 30° |
| Turret Gun Shield | 25.4 mm | 50° |
| Turret Sides/Rear | 25.4 mm | 5°/0° |
| Turret Top | 9.5-19.1 mm | 90° |