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RPG-1

The RPG-1 (Russian: РПГ-1, Ruchnoy Protivotankovy Granatomyot-1, meaning "hand-held anti-tank grenade launcher-1") was the Soviet Union's first domestically developed reloadable, man-portable anti-tank rocket launcher, designed as a lightweight infantry weapon to counter armored vehicles using shaped-charge warheads. It featured a simple 30 mm smoothbore steel tube launcher, approximately 1 meter long and weighing 2 kg when unloaded, that fired 70 mm PG-70 grenades with a muzzle velocity of 40 m/s, achieving effective aimed fire out to 75 meters and armor penetration of up to 150 mm at 100 meters—sufficient to defeat the frontal armor of contemporary tanks like the German Tiger I during trials. Development of the RPG-1 began in early 1944 at the Scientific Research Institute for Chemical Machine-Building (NIPSMVO) under engineer A. Kazanovich, spurred by the Red Army's capture and evaluation of German disposable launchers, rocket launchers, and the American M1 Bazooka during ; initial prototypes, designated LPG-70, were tested between and , with refinements continuing by the SKB . Officially designated 56-G-661 for the launcher and 57-GK-661 for the , it received GAU (Main Artillery Directorate) approval in 1948 after addressing issues like misfires (reduced from 7.9% in early tests) and fouling from gunpowder residue, though full-scale production remained limited due to ongoing improvements. The weapon supported a of 9–12 rounds per minute and was operated by a single soldier, emphasizing portability for units, but its short range and modest penetration prompted rapid iteration into the more powerful by 1949, which became the Soviet standard. Despite its brief service life, the RPG-1 established the foundational layout—involving a reusable tube and rocket-assisted —for subsequent Soviet RPG series, influencing global anti-tank infantry tactics during the .

Development

Early concepts and requirements

During , the faced increasing challenges from heavily armored tanks, prompting the Main Artillery Directorate (GAU) to issue formal requirements on December 11, 1942, for a large-caliber, man-portable anti-tank . This weapon was envisioned to penetrate at least 50 mm of armor at a 60-degree angle from up to 400 meters, while weighing no more than 12 kg and allowing firing from prone, kneeling, or standing positions to enhance mobility on the battlefield. Early Soviet efforts to develop such systems dated back to , exemplified by the crude 65 mm RS-65 shoulder-fired tested in 1931, which ultimately failed due to its excessive weight, poor reliability, and inability to achieve practical battlefield performance. These initial experiments highlighted the technical hurdles in creating a lightweight, effective rocket-propelled anti-tank weapon, leading Soviet designers to prioritize anti-tank rifles like the PTRD and PTRS in the early war years. However, as German armor thickened and deliveries introduced the American to Soviet observers by 1943, interest in reloadable rocket launchers revived. Captured weapons played a pivotal role in shaping Soviet concepts, particularly the German and encountered in large numbers during 1943–1944 operations. Trials of these devices revealed their superior shaped-charge warheads, capable of penetrating 180–230 mm of armor, far exceeding contemporary hand-thrown Soviet grenades like the RPG-43. Combining the 's simplicity with the 's reloadability—inspired also by the —the Soviets aimed for a versatile, infantry-held system that could be produced inexpensively and used effectively against evolving threats. The resulting preliminary design, initially designated LPG-44 (after , the start of formalized work) or LPG-70 (reflecting the projectile caliber), targeted a lightweight, reusable launcher firing a 70 mm shaped-charge to surpass the limitations of single-use grenades. This conceptualization, led by A. Kazanovich's team at the Scientific Research Institute for Chemical Machine-Building (NIPSMVO) with involvement from G.P. Lominskiy, sought to balance portability, ease of reloading, and sufficient range for close-quarters anti-tank engagements.

Design and testing phase

The design and testing of the RPG-1 began in early 1944 under A. Kazanovich at the , building on early requirements established in 1942 for an anti-tank capable of penetrating at least 50 mm of armor at 400 meters with a total weight not exceeding 12 kg. The primary prototype, designated LPG-44 (Light Grenade Launcher), featured a reloadable shoulder-fired launcher paired with the PG-70 shaped-charge , which used a to ignite a 30 mm for initial , followed by rocket motor activation to propel the 70 mm toward armored targets. This aimed to provide Soviet with a lightweight, reusable system for close-range anti-tank engagements, drawing from captured and influences but adapted for simpler production and reliability in field conditions. Initial testing occurred from 1944 to 1945 at Soviet proving grounds, where the LPG-44 demonstrated promising penetration capabilities of 150-200 mm against armor, validating its potential as an effective infantry weapon. However, these trials revealed significant issues with consistency, including unstable burning rates across varying temperatures—from summer heat to winter cold—which led to erratic flight paths and reduced accuracy. In August-September 1945, more extensive evaluations involved 15 launchers and nearly 1,000 PG-70 rounds, achieving consistent 150 mm penetration but with a 7.9% misfire rate, prompting further refinements to address the and ignition reliability. Development continued through 1947-1948, with iterative improvements focused on enhancing and feasibility, including the of an open planar sight for better aiming without a front sight post and the addition of wooden thermal protective overlays on the launcher's barrel to shield the operator from heat during firing. These modifications aimed to balance performance with mass manufacturability using readily available materials. By 1948, the prototype had evolved sufficiently for approval by the Artillery Committee of the GAU, at which point it was officially renamed the RPG-1 (Ruchnaya Protivotankovaya Granata, or Hand Anti-Tank Grenade) to emphasize its role as a system, with the PG-70 .

Technical description

Launcher

The RPG-1 launcher, known as the LPG-70, measures 100 cm in length and 30 mm in diameter, with an empty weight of 2 kg, making it suitable for portable infantry use. It consists of a smoothbore steel tube open at both ends, surrounded by a wooden sheath that protects the operator from heat generated during firing and provides a firm grip. This construction prioritizes simplicity and durability for field conditions during World War II. The firing mechanism features a rear-mounted percussion cap system that strikes the propellant charge to propel the grenade from the muzzle. A basic leaf-type iron sight is affixed to the top of the tube for straightforward point-and-shoot aiming. Designed for single-operator use, the launcher is shoulder-fired from standing, kneeling, or prone positions, with recoil minimized by venting exhaust gases rearward through the open breech, enhancing stability without additional supports. Its lightweight build supports high mobility, allowing a soldier to carry and deploy it rapidly in combat. Reloads occur via front-loading insertion of the into the tube, enabling a practical of 9-12 rounds per minute. Integrated with the PG-70 , the full system weighs 3.6 kg.

Grenade and propulsion

The PG-70 , the primary for the RPG-1, measured 425 mm in length and 70 mm in diameter, with a total weight of 1.6 kg. It featured an over-caliber design, allowing it to fit within the launcher's 30 mm tube while providing enhanced anti-tank capability. The employed a hollow-charge (shaped-charge) configuration filled with , optimized for penetrating medium armor up to 150 mm thick at normal incidence. This design focused explosive energy to create a high-velocity jet capable of defeating armored vehicles, marking an early Soviet adaptation of anti-tank shaped-charge technology. Propulsion was provided by a black powder charge integrated into the , which ignited upon firing to achieve an initial of approximately 40 m/s. The lacked a sustainer motor, relying instead on ballistic after launch, with flight stabilized by a rigid tail stabilizer. Loading occurred from the front (muzzle) of the launcher, with the grenade's aligning for percussion ignition. mechanisms included a basic arming sequence tied to the strike, though specific delay features for premature prevention were not detailed in period designs.

Performance characteristics

Capabilities and limitations

The RPG-1 had an of 75 meters for anti-tank engagement, limited by the low and rudimentary stabilization of the . In terms of penetration, the RPG-1's PG-70 could defeat up to 150 mm of rolled homogeneous armor (RHA) at optimal ranges, sufficient against the side armor of medium tanks like the but marginal against the frontal armor of late-war heavy tanks like the exceeding 100 mm effective thickness. Key limitations included inconsistent rocket quality leading to unstable penetration and flight paths, with a muzzle velocity of 40 m/s. Reliability issues included a 7.9% misfire rate in trials and fouling of the trigger mechanism after 15–30 shots. The short range limited engagements to close quarters, while the total weight of 3.6 kg (launcher plus ) was burdensome for prolonged use. The shaped-charge provided low , aiding operator safety.

Comparison to contemporaries

The RPG-1, with its 70 mm grenade, provided a larger than the M9 Bazooka's 60 mm rocket, potentially enabling higher armor penetration of up to 150 mm compared to the Bazooka's approximately 127 mm. However, the RPG-1's was limited to 75 m, shorter than the Bazooka's 110 m, and its proved less reliable, with trials showing a 7.9% misfire rate. In comparison to the German , the RPG-1 shared a similar shoulder-fired, reloadable design but lacked the 's protective blast shield, exposing operators to greater backblast risk. The RPG-1's maximum of 75 m also fell short of the 's 150 m, though its lighter weight of 2 kg (unloaded) offered better portability compared to the 's 9.5–11 kg. The RPG-1 sought to address the 's disposable nature by introducing reloadability, allowing sustained fire in combat, but it retained a similarly short of around 75 m versus the Panzerfaust 60's 60 m. While the RPG-1 achieved 150 mm penetration, this did not match the later variants' up to 200 mm, and the added mechanical complexity reduced its simplicity without proportional gains in performance. Overall, the RPG-1 represented a Soviet effort to adapt captured and designs for inexpensive mass production using simple materials like black powder, but its rushed late-war development led to reliability issues that made it less effective than contemporaries in comparative trials, ultimately limiting its adoption.

Adoption and legacy

Reasons for cancellation

The RPG-1 encountered significant technical challenges during late-stage evaluations, particularly with its propellant system, which proved unreliable and led to erratic flight paths and frequent misfires. In trials conducted between 1945 and 1948, the rocket's inconsistent quality resulted in a 7.9% misfire rate across 750 launches, with the trigger mechanism after just 15-30 shots, often causing jams that failed to meet the GAU's reliability standards for wartime deployment. Performance metrics further undermined the weapon's viability, as its shaped-charge warhead achieved only marginal armor penetration of approximately 140-150 mm at 100 meters, while the effective range was limited to about 75 meters. Logistical drawbacks compounded these problems, with the RPG-1's design requiring over 660 pages of blueprints across 40 albums for production, indicating higher complexity than desired for rapid mass issuance during wartime. Additionally, the inclusion of wooden components, such as protective pads on the launcher to mitigate barrel heat, made the system vulnerable to environmental factors like moisture and temperature fluctuations, complicating field maintenance and storage. The end of in 1945 shifted Soviet military priorities away from rushed anti-tank developments, allowing for more deliberate evaluation. By 1947, parallel work on the RPG-2 prototype demonstrated superior reliability, range, and penetration, leading to the RPG-1's cancellation in 1948 without entering production or service.

Influence on subsequent weapons

Despite its cancellation, the RPG-1's design elements directly influenced the development of its successor, the , which was adopted by the in 1949. The retained the RPG-1's 70 mm caliber and shaped-charge warhead concept, derived from the PG-70 grenade, but addressed key propulsion flaws through a more reliable booster charge using subdivided black powder increments, extending effective range to approximately 200 meters. The RPG-1's emphasis on lightweight, infantry-portable launchers and reloadable tube mechanisms provided foundational lessons that shaped the evolution of later systems, including the introduced in 1961. This progression maintained the core reloadable design while upgrading to rocket-assisted propulsion for the PG-7 series of grenades, which built upon the PG-70's shaped-charge principles to achieve greater velocity and penetration. Through its 1945-1948 trials, the RPG-1 validated the viability of rocket-propelled grenades within Soviet anti-tank , paving the way for widespread adoption of similar systems in export designs and among allies, though no direct variants of the RPG-1 were produced due to its program's termination.

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