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RP-3

The RP-3 was a British air-to-ground rocket projectile introduced during the Second World War. The "3 inch" designation referred to the nominal diameter of the rocket motor tube. The use of a 60 lb (27 kg) warhead gave rise to the alternative name of the "60-pound rocket". Though an air-to-ground weapon, it saw limited use in other roles. They were generally used by British fighter-bomber aircraft against targets such as tanks, trains, motor transport and buildings, as well as by Coastal Command and Royal Navy aircraft against U-boats and ships.

History
Earlier systems The first use of rockets fired from aircraft was during the First World War. The "unrotated projectiles" (UPs) were Le Prieur rockets mounted on the interplane struts of Nieuport fighters. These were used to attack observation balloons and were reasonably successful. Sopwith Baby, Sopwith Pup and Home Defence B.E.2 fighters also carried rockets. Development Starting in 1935, the British began development of new anti-aircraft weapons, including cordite-powered surface-to-air rockets. Several models of these Unrotated Projectile (UPs) were introduced, starting with a diameter model that saw use both in ground batteries and on larger ships. In 1937, new models at and diameters were introduced. By 1938, work on the 2-inch model had been slowed in favour of the 3-inch models which offered performance similar to the QF 3-inch 20 cwt anti-aircraft gun. Tests in Bermuda in 1939 suggested that the accuracy was not high enough to be used in a fashion similar to a gun, and development was slowed. After the Dunkirk evacuation in 1940 it was clear an attack on the UK was coming, and production was quickly ramped up. Still considering the accuracy to be low, they were to be fired in salvos from the "Z-Batteries". Information was sought from the Soviets, who had been using unguided RS-82 rockets since 1937. By September 1941 it was decided that two models of UP would be developed: • A 23 lb plastic explosive on a standard 2-inch UP • A 20 lb solid armour-piercing head on a 3-inch UP When it was realised that the 2-inch version would be less effective than the Vickers S cannon, it was decided to concentrate on development of the 3-inch version, which could be developed from the 3-inch rocket used in the Z-Batteries. == Design ==
Design
The rocket body was a steel tube in diameter and long filled with of cordite propellant, fired electrically. The warhead was screwed into the forward end, and was initially a solid , diameter and long (with adaptor) armour-piercing warhead which was quickly supplanted by a , high explosive head. induced enough spin to stabilize the rocket, but as it was unguided, aiming was a matter of judgment and experience. Approach to the target needed to be precise, with no sideslip or yaw, which could throw the RP off line. Aircraft speed had to be precise at the moment of launch, and the angle of attack required precision. Trajectory drop was also a problem, especially at longer ranges. The rocket was less complicated and more reliable than a gun firing a shell and there was no recoil on firing. It was found to be a demoralising form of attack against ground troops and the 60-pound warhead could be devastating. The rocket installations were light enough to be carried by single-seat fighters, giving them the punch of a cruiser. Against slow-moving large targets like shipping and U-boats, the rocket was a formidable weapon. The weight and drag of the all-steel rails initially fitted to British aircraft blunted performance. Some aircraft such as the Fairey Swordfish biplane used against submarines had steel "anti-blast" panels fitted under the rails to protect the wing, which further increased weight and drag. Aluminium Mark III rails, introduced from late 1944, reduced the effect. American experience with their own rockets (the USAAF's 3.5-Inch Forward Firing Aircraft Rocket (FFAR) and the US Navy's 5-inch FFAR and HVAR) showed that the long rails and anti-blast panels were unnecessary; zero-length launchers were introduced in May 1945. British aircraft started being fitted with "zero-point" mounting pylons in the post-war years. The 3-inch rocket motors (less warhead) were used in the 'bunker buster' "Disney bomb" (official name: 4500 lb Concrete Piercing/Rocket Assisted bomb), 19 of them propelling the bomb to at impact with the target. == Service history ==
Service history
Air-to-ground use photo of a rocket salvo fired at railway wagons in a siding at Nordhorn, Germany (1945) Before the new weapon was released for service extensive tests were carried out by the Instrument, Armament and Defence Flight (IADF) at the Royal Aircraft Establishment, Farnborough. Hawker Hurricanes were fitted with rockets and rails and flown during June and July 1942. Further tests were undertaken from 28 September to 30 November to develop rocket-firing tactics. Other aircraft used were a Lockheed Hudson, a Fairey Swordfish biplane torpedo bomber, a Douglas Boston medium bomber and a Sea Hurricane. For rockets only the Mk IIIA was the most successful – it was used on the Lockheed Ventura and Hudson. The first operational use of the RP was in the Western Desert campaign as a "tank-busting" weapon on Hawker Hurricane Mk. IIEs and IVs. The 25-pound armour-piercing heads were found to be ineffective against the Tiger I heavy tanks coming into German service. With the example of the success of Royal Artillery gunners using high-explosive shells from their Ordnance QF 25 pounder gun-howitzers, it was decided to design a new 60-pound semi-armour-piercing (SAP) head. These were capable of knocking turrets off tanks. A typical RP-3 installation was four projectiles on launching rails under each wing. A selector switch was fitted to allow the pilot to fire them singly (later omitted), in pairs, or as a full salvo. Towards the end of the war some RAF Second Tactical Air Force (2 TAF) Hawker Typhoons had their installation adapted to carry an additional four rockets doubled up under the eight already fitted. RP-3s were widely used during the battle the Falaise pocket in mid-August 1944. During the battle German forces, retreating to avoid being trapped in a pincer movement by Allied ground forces, came under air attack. Amongst the waves of light, medium and fighter bombers attacking the German columns the Typhoons of 2 TAF attacked with their rockets, claiming hundreds of tanks and "mechanised enemy transport". After the battle, Army and 2nd TAF Operational Research Sections studying the battleground came to the conclusion that far fewer vehicles, 17 in total, had been destroyed by rocket strike alone. What was clear was that in the heat of battle it was far harder for pilots to launch the weapons while meeting the conditions needed for accuracy. Smoke, dust and debris in the target areas made accurate assessment of the damage caused almost impossible. Anti-submarine . Soon after some encouraging results from the initial deployment, trials of the weapon were conducted against targets representing U-boats. It was discovered that if the rockets were fired at a shallow angle, near misses resulted in the rockets curving upwards in seawater and piercing the targets below the waterline. Soon Coastal Command and the Royal Navy's Fleet Air Arm aircraft were using the rockets extensively. The first U-boat destroyed with the assistance of a rocket attack was U-752 (commanded by Schroeter), on 23 May 1943, by a Swordfish of 819 Naval Air Squadron (819 NAS). The rockets used on this occasion had solid, cast-iron heads and were known as "rocket spears". One of these punched right through the submarine's pressure hull and rendered it incapable of diving; the U–boat was scuttled by its crew. On 28 May 1943, an RAF Hudson of 608 Squadron destroyed a U-boat in the Mediterranean, the first destroyed solely by rocket. The rockets were highly inaccurate when fired from a tank as they were being fired from a stationary point and had little slipstream over the fins. Despite this, the RP-3 was valued by tank crews for the destructive effect of its 60-pound warhead. In combat, they were also used for short-range, saturation bombardment of an area and were effective as an immediate counter to German ambushes. to 1957. Sweden had been experimenting with caseless ammunition as a substitute for air-to-ground rockets during WWII as it was thought that caseless ammunition would be cheaper to produce. This however proved false and by the end of the war the Swedish air force had moved to rocket development instead. The remaining 8 cm prak m/46B rockets were modified with new sloped fins around 1953. Around 30% of the fin surface area was removed. This decreased the chance of the fins breaking off during launch and also increased accuracy. These fins were designated ' and when equipped on the ' the suffix changed to C, then becoming (8 cm prak m/46C). The 8 cm prak m/46C remained in service until 1957. During its service life in the Swedish air force the rocket came to serve on several Swedish aircraft. To allow universal usage of the RP-3 the first and second generation of Swedish air-to-ground rockets used the same mounting system as the RP-3. == Variants ==
Variants
Warheads ;Shell, 18 lb, HE : "high-explosive" warhead. ;Shot, 25 lb, AP, No. 1, Mk. I :Armour-piercing warhead made out of hardened steel. Used against submarines and merchant ships at angles of 15 degrees or greater. ;Shot, 25 lb, AP, No. 2, Mk. I :Improved design over the Shot, 25 lb, AP, No. 2, Mk. I warhead made longer and pointier to increase penetration. By 1946 the design was obsolete and only used for advanced training. fitted to the nose, the whole warhead was long and weighed . The relatively thick wall ( 0.85 inches) and high explosive (TNT or RDX/TNT) filling produced "heavy fragments" which inflicted damage at "considerable distance". ;Shell, HE, 60 lb, SAP :Semi-armour-piercing high-explosive warhead that existed in four primary variants: :*Shell, HE, 60 lb, SAP, No. 1, Mk. I :*Shell, HE, 60 lb, SAP, No. 2, Mk. I :*Shell, HE, 60 lb, SAP, No. 1, Mk. II :*Shell, HE, 60 lb, SAP, No. 2, Mk. II :Variants designated mark 1 (Mk. I) had a shell body that consisted of two parts that were screwed together, a body and a tip. Variants designated mark 2 (Mk. II) had the aforementioned shell body and tip forged together as one piece. Variants designated number 1 (No. 1) were fitted with a time delayed base fuze (Fuze, No. 865, Mk. I) that allowed them to penetrate into a target before detonating. ;Shell, Practice, Concrete, 60 lb Mk. I :Practice warhead 20 in long by 6 in diameter formed of concrete over steel reinforcing rods. Used to simulate shooting the 60 lb SAP/HE warheads. This warhead could also be fitted with the "Smoke container, No. 1, Mk. I", which pressed on over front of the warhead and gave off a smoke signal on impact. The filling was of titanium tetrachloride. ;Shell, HE, 60 lb, G.P. :High-explosive general-purpose (Hollow charge) warhead, trials ongoing as of September 1946. Rocket engines The RP-3 rocket engine was updated a number of times during its lifespan, which gave rise to a number of variants. For example, it was necessary to modify the rocket engine's propellant charge in order to be able to use several types of warheads. Initially the rocket engine was only designed to use warheads up to , but when warheads up to were introduced the propellant charge had to be modified in order to use them. Variants capable of carrying warheads up to 60 lb were then given the supplementary designation TH after the mark number. ;Aircraft rocket motor, 3 in., No. 1, Mk. 1 :The Mk. 1 engine had a tubular-shaped cordite propellant charge. The ignition cables are routed through the tubular propellant charge. This variant was suitable for use with 25 lb solid warheads. ;Aircraft rocket motor, 3 in., No. 1, Mk. 1/TH :TH variant of the Mk. 1 engine that could mount solid or shell warheads up to 25 lb. It could likewise not be used in hot climates. ;Aircraft rocket motor, 3 in., No. 1, Mk. 2/TH :TH variant of the Mk. 2 engine that could mount warheads up to 60 lb. During storage the extra length of the ignition cables was held in place by loose metal clips in the nozzle. Comparison == Aircraft use in the Second World War ==
Aircraft use in the Second World War
As well as operational use, a number of aircraft were fitted with RP-3s on an experimental basis. RAF and Commonwealth air forces Boeing Fortress Mk. II and IIA: (Coastal Command) • Bristol Beaufighter Mk. VI, VIC, X and 20: (Coastal Command, South East Asia Command and Royal Australian Air Force, Pacific Theatre.) • Consolidated Liberator B. Mk. III, VI: (Coastal Command.) • de Havilland Mosquito F.B. Mk. VI: (Coastal Command, SEAC and RAAF, Pacific Theatre.) • Hawker Hurricane Mk. IIE & IV: (Desert Air Force, RAF Second Tactical Air Force, SEAC.) • Hawker TempestHawker Typhoon Mk. Ib: (2 TAF.) • Republic P-47 Thunderbolt (USAAF used their M8 for this role instead, 6/aircraft) • Supermarine SpitfireVickers Wellington GR Mk. XIV: (Coastal Command) Royal Navy Fleet Air Arm Fairey Firefly Mk. I • Fairey Swordfish Mk. II, III • Grumman Tarpon/Avenger Mk. I, II, III • Hawker Sea Hurricane Mk. IIc (825 Naval Air Squadron) • Hawker Sea Fury 807 Naval Air Squadron == Aircraft use post Second World War ==
Aircraft use post Second World War
The 3-inch RP continued to be used on RAF and RN aircraft in the ground attack role until replaced by the SNEB podded rocket (RAF) and the 2-inch podded RP (RN). Post war operational use included the Malayan emergency, the Korean War, the Suez Crisis, and the Radfan campaign. RAF and Commonwealth air forces Bristol Brigandde Havilland Hornetde Havilland Vampirede Havilland VenomGloster MeteorHawker Hunter RAAF, RAN RP-3 rockets were used by Australian armed forces into the 1970s • Bristol Beaufighter • North American P-51 Mustang • de Havilland Vampire • Fairey Firefly • Gloster Meteor • Fairey Gannet • Hawker Sea Fury Mk11 • de Havilland Sea Venom Royal Navy Fleet Air Arm Hawker Sea FuryHawker Sea HawkSupermarine AttackerSupermarine Scimitarde Havilland Sea Vixen - up to 24 rockets total on 4 pylons, six per pylon; Swedish Air Force North American T-6 Texan (Sk 16) - 4 rockets total on 2 pylons • Saab 17 (B 17A) - 4 rockets total on 4 pylons) • Saab 18 (A & T 18B) - 8-12 rockets total on 8-9 pylons • Saab 21 (A 21A-3) - 8 rockets total on 2 pylons) • Saab 21R (A 21RA, RB) - 10 rockets total on 1 pylon • de Havilland Vampire (J 28B, C) - 8 rockets total on 4 pylons • Saab 29 Tunnan (J 29A, B, E, F) - 8 rockets total on 8 pylons • Saab 32 Lansen (A 32A) - 12 rockets total on 12 pylons == See also ==
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