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M3 howitzer

The 105 mm M3 was a lightweight, towed piece developed by the for airborne troops during , featuring a shortened barrel from the existing M2 howitzer mounted on a modified from the 75 mm M1A1 pack howitzer to enhance portability. Weighing 1,130 kg (2,491 lb) and manned by a of 5 to 10, it had a barrel length of 1.68 m (16 calibers), a maximum range of 7.6 km (8,300 yards) with high-explosive shells, and a up to 4 rounds per minute (sustained at 2 rounds per minute). Designed in 1941 as the T7 to meet the need for compact that could be air-dropped or transported by glider, the M3 was tested at in March 1942 and standardized in 1943 on the M3 carriage. Production ran from February 1943 to June 1945, yielding 2,580 units manufactured in the United States, with annual outputs of 1,965 in 1943, 410 in 1944, and 205 in 1945. It fired semi-fixed types including high-explosive, high-explosive antitank, smoke, and illumination rounds, with a of 311 m/s (1,020 ft/s). The M3 entered combat in June 1944 with U.S. airborne divisions during the , providing close support fire for regiments and paratroopers in operations like on , . It equipped cannon companies in divisions and battalions of the 82nd and 101st Divisions, offering capabilities up to 7,600 meters despite its reduced power compared to standard 105 mm . Post-war, it was exported in limited numbers—94 to Free French forces, 2 to , and 18 to Latin American countries—and saw variants like the M3A1 and M3A2, though it was eventually phased out as obsolete by the late 1940s.

Design and specifications

Barrel and ballistics

The barrel of the M3 howitzer was derived from the howitzer tube, shortened by 27 inches to reduce weight and enhance air-transportability for operations. This modification resulted in a bore length of approximately 1.68 meters (16 s overall), with the full barrel assembly measuring about 1.88 meters. The is 105 mm (4.13 in), featuring uniform with a right-hand twist of one turn in 20 calibers. Ballistic performance includes a muzzle velocity of 311 m/s (1,020 ft/s) using the standard charge with the M1 high-explosive shell. The maximum range reaches 7,600 meters (8,300 yards) at 45° elevation, limited by the weapon's design priorities for lightness over long-range power. Elevation limits vary by carriage, from -9° to +30° (up to +45° on some variants), with a total traverse of 46°. The recoil system employs a hydropneumatic (M13 or type) with a hydraulic and recuperator, designed for constant and absorbing approximately 30 inches (76 cm) to maintain stability during firing. The barrel and breech together weigh about 995 pounds (451 kg), contributing to the overall lightweight profile when integrated with the for airborne deployment.

Carriage and mobility

The M3 howitzer employed a split-trail carriage designated as the M3 or M3A1, adapted from the design of the 75 mm pack howitzer carriage to accommodate the 105 mm barrel while maintaining lightweight construction for airborne deployment. The M3A1 variant featured reinforced steel trails for enhanced durability during rough handling. This high-speed carriage type used wheel carriers with automobile disk and rim wheels, enabling efficient transition between traveling and firing positions via simple pivoting of the trails. In the firing position, the complete howitzer and carriage weighed 2,495 (1,130 ) without accessories, providing a balance of portability and through a three-point ground contact system involving spades on the trails and the firing baseplate. For transport, the trails were closed and locked, distributing the weight to the wheels at approximately 1,193 on the right and 1,198 on the left, for a total of about 2,391 (1,085 ). The carriage incorporated pneumatic tires sized 8.00 x 16 with a recommended of 30 , fitted with combat-type beadlocks for off-road resilience. It was typically towed by a quarter-ton or similar light vehicle, with hand brakes for secure parking during movement. Mobility was optimized for airborne operations, transported intact via glider, with quick emplacement on the drop zone using manpower or light vehicles like jeeps for relocation over rough terrain. In the firing configuration, the split trails opened to support a maximum traverse of 22°30' to either side via the manual traversing mechanism. The M3A2 carriage variant included an optional small 14-gauge shield mounted forward to offer limited protection to the crew from blast and small-arms fire. Emplacement from transport to ready-to-fire position could be achieved in approximately 5 minutes by a gun section.

Development and production

Design origins

The development of the M3 105 mm howitzer was initiated in 1941 by the U.S. Army Ordnance Department to meet the growing requirements of airborne divisions for a lightweight pack artillery piece capable of supporting parachute and glider operations. This effort responded to the need for artillery that could be rapidly deployed behind enemy lines without reliance on ground transport, emphasizing air portability for units like those tested at Fort Bragg. The design drew directly from the existing M2 105 mm howitzer, adapting its barrel by shortening it from 22 calibers to 16 calibers—a reduction of about 27 inches—to enhance compactness while maintaining ballistic compatibility. The prototype, designated the 105 mm Gun T7 mounted on M1A1, incorporated the shortened M2 barrel with the lighter recoil mechanism and split-trail derived from the 75 mm pack M1A1 to achieve the necessary reductions in size and weight. Key objectives included limiting the overall weight to under 2,500 pounds (approximately 1,134 kg), ensuring compatibility with glider transport such as the , and allowing full interchangeability with standard 105 mm M2 ammunition for logistical simplicity. This approach prioritized mobility for , enabling disassembly into loads suitable for or glider delivery while preserving effective firepower. Testing of the T7 prototype commenced at in March 1942, where it demonstrated reliable performance, including a maximum range of around 7,000 meters and manageable recoil through the adapted 75 mm system. Following successful evaluations that confirmed its air-transportable design and operational viability, the weapon was standardized as the M3 howitzer in 1943.

Manufacturing details

The production of the M3 howitzer occurred from to 1945, with a total of 2,580 units manufactured to support and light needs during . Initial production began in February and ran continuously until May 1944, followed by a smaller batch from April to June 1945 to meet late-war demands. Annual output peaked in the first year at 1,965 units in , declining to 410 units in 1944 and 205 units in 1945 as wartime priorities shifted. Barrels for 105 mm howitzers were produced at the in , the U.S. Army's primary facility for manufacturing large-caliber gun tubes, which supplied components for various artillery pieces including the M2 series from which the M3 was derived. The design emphasized modular assembly, adapting the shortened M2 barrel to the lightweight M1 pack howitzer carriage for rapid wartime scaling and ease of transport by . Other components, such as the carriage elements, were handled by U.S. Army Ordnance Department facilities including . Quality control involved rigorous post-production testing at arsenal facilities for accuracy, durability, and ballistic performance, ensuring high reliability in combat conditions; Watervliet's processes during this period achieved near-complete interchangeability of parts and a 99.5% on-time completion rate for cannon production. Production ceased in mid-1945 due to the conclusion of and the U.S. Army's transition to the heavier, more versatile for general roles, rendering the specialized M3 less essential beyond airborne units.

Operational history

World War II

The M3 105mm saw extensive service with U.S. forces in the European Theater during , particularly among and units requiring lightweight, transportable for rapid deployment. It equipped cannon companies in regiments, such as the 90th Division, and field battalions in divisions like the 82nd and 101st, providing close in fluid combat environments. Designed for air-transportability, the weapon could be disassembled for delivery by or glider, enabling quick assembly behind enemy lines to deliver . In the Normandy campaign following the D-Day landings of June 6, 1944, the M3 supported airborne operations and subsequent infantry advances, with gunners from the 90th Infantry Division firing the howitzer near on June 11 to repel German counterattacks during intense hedgerow fighting. The weapon's short barrel and reduced-power rounds allowed effective direct and indirect support up to 7,600 meters, aiding in breaking enemy positions while minimizing logistical burdens for mobile forces. Airborne units, including elements of the , integrated the M3 into their glider battalions for post-landing fire missions, using standard high-explosive shells to target fortifications and troop concentrations. During in September 1944, the 319th Glider Field Artillery Battalion of the employed M3 howitzers to defend key bridgeheads, notably on Finger Ridge near . Positioned within 75 yards of forward lines, the guns delivered precise, single-round adjustments and full-battery barrages, including phosphorous shells to disrupt German advancing with tanks, ultimately repelling multiple assaults and securing the ridge against superior enemy numbers. This close-support role highlighted the M3's versatility in defensive airborne operations, where rapid setup and high-angle fire were essential for holding tenuous positions. In the during December 1944, the M3 proved vital in the defense of , where the 907th of the fired from positions as close as 1,000 yards behind the lines to halt German advances near Neffe and Marvie. Amid ammunition shortages that limited daily firing to 10 rounds per gun by , the howitzers targeted tanks and infantry in massed barrages, contributing to the destruction of multiple armored vehicles and repelling assaults until resupply arrived on December 23. Atmospheric adjustments enhanced accuracy despite overcast conditions, underscoring the weapon's reliability in prolonged siege warfare; forward observers suffered heavy casualties, with the battalion losing four killed in the effort. The 463rd Parachute also used M3s on Day to stop two German tanks at 600 yards in the 327th sector, aiding in disabling 18 enemy vehicles overall. A limited number of M3 howitzers were provided through to Allied forces, including the Free French. By 1945, over 2,500 M3s had been produced, with the majority serving U.S. units in to bolster airborne and infantry firepower.

Post-World War II

Following , the M3 howitzer saw limited continued service, primarily in the early stages of the (1950–1953). The (ROK) was equipped with the M3 105 mm howitzer, which had been supplied as part of U.S. ; by mid-1950, ROK forces had five battalions outfitted with these weapons, each battalion comprising three firing batteries of five howitzers for a total of 75 guns, with 91 units on hand and 89 serviceable. These were employed by ROK divisions in defensive roles along the 38th Parallel and during initial counterattacks, such as those by the ROK 3rd Division in the Yongdok battles in July 1950, providing close fire support with a maximum range of approximately 8,200 yards. Additional shipments bolstered stocks, including 12 howitzers and 105,000 rounds of ammunition dispatched to Pusan in late June 1950, though some allocations intended for ROK units were diverted to U.S. forces. A modified M3A2 variant remained in operational use by ROK divisions until 1951, marking the howitzer's final combat deployments. In the U.S. military, the M3 was largely retired at the end of , phased out during the 1950s in favor of the more versatile M101 105 mm howitzer, which offered improved range and mobility for standard roles. Remaining stocks were held in reserve, including with units, but were gradually demobilized through the 1960s as priorities shifted toward self-propelled and heavier systems. Surplus M3 howitzers from U.S. inventories were exported in small numbers to allied nations, though no significant post-Korean War combat use was recorded. By the , maintenance challenges arose due to the obsolescence of parts for the lightweight, airborne-optimized design, leading to high attrition rates from wear and eventual scrapping of most remaining units. As of 2025, no M3 howitzers remain in active U.S. or foreign , though preserved examples are displayed in museums, such as at the Rock Island Arsenal, where they highlight World War II-era airborne artillery innovations. Modified versions continue ceremonial use in U.S. Army batteries, firing blank rounds for official events.

Variants

Towed variants

The towed variants of the M3 howitzer encompassed modifications to the gun tube and carriage to better suit , , and rugged terrain operations during . These upgrades addressed limitations in elevation, durability, and crew protection without altering the core design's lightweight profile, which weighed 1,130 kg (2,491 lb) in firing position. Gun variants included the T7, the initial prototype tested in 1941 and standardized as the M3 in 1943, offering a maximum elevation of 30 degrees for high-angle fire in support of units. The T10 variant, developed in 1944, featured an adjusted mount that attempted to increase elevation to 65 degrees to enhance range and precision for missions, but it remained a test model and was not adopted. Both gun types utilized a shortened version of the M2A1 105 mm barrel, ensuring compatibility across towed configurations. Carriage variants began with the standard , a split-trail design adapted from the 75 mm pack carriage, which allowed rapid setup and towing by light vehicles or even manpower in airborne drops. The carriage, introduced in 1944, incorporated stronger trails constructed from 3.2 mm (1/8 inch) plate rather than the original 2.4 mm (3/32 inch), providing greater structural integrity for operations in uneven or muddy conditions. The carriage, produced in limited quantities during 1945, added a protective to safeguard the crew from small-arms fire and in forward positions. All towed variants remained interchangeable with the M2A1 barrel assembly and underwent no significant redesigns after the 1943 , facilitating streamlined and . Total of the M3 reached 2,580 units between 1943 and 1945, with the majority allocated to U.S. divisions.

Self-propelled variants

The T38 105 mm Motor Carriage was proposed in late 1941 by the U.S. Ordnance Department as an experimental self-propelled mount for a light 105 mm on the M3 half-track , intended as an interim solution for mobile support amid concerns that heavier standard would overload the platform. The design aimed to integrate the lighter T7 pack —predecessor to the standardized M3—to enable rapid deployment with units, but the was rejected early due to anticipated stresses on the half-track's and the realization that the could handle full-sized after initial tests. No prototypes were constructed, and the initiative was terminated by March 1942 in favor of more viable alternatives like the T19, which successfully mounted a standard 105 mm on the same . Development of the T82 105 mm Howitzer Motor Carriage began in November 1943 at the , following orders to adapt the M3 howitzer for a compact self-propelled role on the M5A1 chassis, primarily to provide mechanized in the Pacific theater where lighter, more agile vehicles were prioritized. Two prototypes were completed by mid-1944 through collaboration between Massey-Harris and the Heil Company, featuring an open-top turret with 360-degree traverse for the M3 howitzer in Mount M3A1, thin 12.7 mm armor sufficient only against small-arms fire, and a of four. The vehicle weighed approximately 14.5 tons when loaded, carried up to 58 rounds of 105 mm ammunition, and achieved a top speed of around 35 mph on roads, with the howitzer maintaining its standard maximum range of 7,600 meters. Testing commenced in late 1944 at , where the prototypes demonstrated a burst firing rate of up to 4 rounds per minute and satisfactory mobility comparable to the base M5A1 tank, but evaluations at in early 1945 highlighted vulnerabilities including inadequate protection and stability issues during off-road maneuvers on uneven terrain. The program was ultimately cancelled on June 21, 1945, as the end of reduced the need for additional specialized artillery, and existing platforms like the were deemed sufficient for mechanized support, rendering the T82's logistical demands—such as limited ammunition storage and complex turret integration—unviable for widespread adoption. Both prototypes were scrapped following trials, with no units entering production or service.

Ammunition

Projectile types

The M3 howitzer employed semi-fixed 105 ammunition, sharing the same projectile designs as the M2 howitzer series for logistical compatibility. These projectiles were loaded separately from their charges, allowing for adjustments in range through variable charge increments. Shell weights typically ranged from 15 to 19.6 kg, ensuring uniformity across types for consistent handling and in airborne operations. The primary ammunition was the high-explosive (HE) , a forged weighing 14.97 kg (33 lb) with a 2.18 kg (4 lb 13 oz) filler of or 50/50 . Designed for blast and fragmentation effects, it served as the standard round for anti-personnel and suppression, producing an effective burst radius of approximately 30 m against exposed troops. It was fuzed with point detonating (PD) types like the M48 for or superquick airburst , or variable time (VT) proximity fuzes such as the M4 for optimal dispersal over area targets. For dual-role capability against armored threats, the () M67 shell was introduced in 1944, featuring a 2.3 shaped-charge filler in a 13.25 (29.22 lb) . This fixed-round design achieved armor penetration of up to 102 mm at 0° obliquity, enabling support against light and medium while retaining HE-like effects on soft targets. It utilized base-detonating fuzes like the M529 for reliable shaped-charge initiation upon impact. Smoke rounds provided screening and marking functions without chemical agents, as no standardized chemical projectiles were developed for the M3. The white phosphorus (WP) series, weighing 15.56 kg (34 lb) total with a 1.84 kg (4 lb) WP filler, burst on impact to disperse burning particles for immediate screening and limited incendiary effects, fuzed with PD types for ground burst. For persistent clouds, the base-ejection (BE) high-concentration (HC) shell, at 18.29 kg (40 lb), expelled hexachloroethane-zinc canisters via a mechanical time , creating obscuration lasting 40-90 seconds over several hundred meters. Illuminating rounds supported night operations with the M314 projectile, a base-ejection type reaching up to 7 km range to deploy a parachute-suspended flare providing 450,000-600,000 candlepower for 60 seconds, illuminating areas up to 1,000 m altitude. It employed mechanical time fuzes like the M565 for timed ejection, enhancing observation and targeting in low-light conditions. VT fuzes were also compatible across HE and illuminating types for airburst precision.
Projectile TypeDesignationProjectile WeightFiller Weight/TypeKey PerformancePrimary UseCompatible Fuzes
High-Explosive14.97 (33 )2.18 /Burst radius ~30 mAnti-personnel/ (M48), VT (M4)
HEATM6713.25 (29.22 )2.3 102 mm penetration at 0°Anti-armor/dual-roleBase-detonating (M529)
Smoke ()M60 series15.56 (34 )1.84 Immediate screening cloudObscuration/incendiary
Smoke (HC BE)18.29 (40 )HC-zinc mixture40-90 s persistent smokeScreening/markingMechanical time
IlluminatingM314~16.8 Illuminant mix7 km range, 60 s burnNight illuminationMechanical time (M565), VT

Propellant and performance

The M3 howitzer employed the incremental M1 series propelling charges, consisting of a base charge and six removable increments numbered 1 through 7, composed of single-base packaged in cloth bags for adjustable . These charges allowed gunners to select the appropriate increment based on desired and , with the full charge 7 delivering a of 311 m/s (1,020 ft/s) when firing standard 105 mm M1 high-explosive projectiles. Range performance varied significantly with charge selection and elevation; for instance, charge 1 at low-angle fire achieved approximately 3,000 m, while the maximum range with charge 7 reached 7,600 m at 43° elevation. The weapon's sustained was 2 rounds per minute for prolonged engagements, with short bursts capable of 4 rounds per minute to maintain barrel cooling and crew efficiency. Muzzle kinetic energy with full charge approximated 725 kJ per round, derived from the 15 kg projectile mass and 311 m/s velocity, though the system's design prioritized lightweight portability over higher-energy outputs. Recoil energy was managed at approximately 34 kJ (25,000 ft-lb), absorbed by a hydropneumatic mechanism to minimize disruption during airborne operations. Safety constraints limited maximum chamber pressure to 28,000 psi, preventing the development of supercharges that could exceed the light barrel's stress tolerance.

Operators

United States

The adopted the 105 mm M3 in 1943 specifically for airborne operations, issuing it to select field artillery battalions such as the 320th Glider Field Artillery Battalion starting in 1944 to provide enhanced firepower over the earlier 75 mm pack howitzers. It was also allocated to light divisions, including the , where its lightweight construction—totaling 1,130 kg in firing position—enabled transport via glider or disassembly for airdrop. This adoption addressed the need for a compact 105 mm weapon capable of supporting paratrooper assaults with a maximum range of 7,620 meters. Organizationally, airborne units integrated the M3 with six guns per and twelve per , allowing for concentrated in fluid scenarios. Training at , —the primary hub for —emphasized disassembly into loads for delivery and rapid reassembly, with focusing on emplacement times under five minutes to enable immediate responsiveness. By 1945, U.S. inventories exceeded 2,500 M3 howitzers, with total production reaching 2,580 units to equip and light formations amid wartime demands. The weapon contributed to combat efforts in and the Pacific, delivering critical during key assaults. The M3 was phased out of service by 1948, supplanted by the heavier 105 mm for its superior range and payload in non-airborne roles. Surviving stocks lingered in reserve formations and training units until the final documented U.S. instructional use in 1955, after which it was fully retired.

Foreign users

The M3 howitzer was distributed to several non-U.S. operators through the Lend-Lease program during World War II and subsequent surplus transfers, totaling approximately 164 units across various nations. These transfers supported Allied efforts and post-war defense needs, with the lightweight design proving suitable for training, evaluation, and limited combat roles in diverse terrains. The United Kingdom received 2 units via Lend-Lease for evaluation and training purposes, with no combat deployment recorded. These howitzers allowed British forces to assess the weapon's airborne and infantry support capabilities without broader adoption. France obtained 94 units for the Free French forces, which were employed during the Italian Campaign in 1944 and the . The transfers formed part of broader aid that equipped eight French divisions with U.S. munitions. In , 18 units were distributed to various countries, including , primarily for border defense and training into the . integrated the M3 into light infantry support roles, leveraging its pack howitzer features for regional operations. South Korea received over 50 units from U.S. surplus, which saw active use during the , including with the Republic of Korea () 5th Division for close infantry support. The M3 served as the main artillery for battalions early in the conflict due to its lightweight design, before retirement in the 1960s. Additional post-war transfers went to countries including , the , and for training and reserve use. The received units as post-1945 aid, where the howitzer continued in service for training and exercises into the 2010s, as demonstrated in joint operations like Exercise 2015.

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