R4M: Difference between revisions
Added template |
|||
Line 80: | Line 80: | ||
* [https://web.archive.org/web/20160101174515/http://www.deutscheluftwaffe.de/archiv/Dokumente/ABC/f/Flakraketen/R4M%20Orkan/R4M%20Orkan.html German language page on details of the R4M unguided rocket, and its ''Panzerblitz'' ground attack version] |
* [https://web.archive.org/web/20160101174515/http://www.deutscheluftwaffe.de/archiv/Dokumente/ABC/f/Flakraketen/R4M%20Orkan/R4M%20Orkan.html German language page on details of the R4M unguided rocket, and its ''Panzerblitz'' ground attack version] |
||
{{Use dmy dates|date=June 2017}} |
{{Use dmy dates|date=June 2017}} |
||
{{WWIIGermanAerialWeapons}} |
|||
[[Category:Air-to-air rockets of Germany]] |
[[Category:Air-to-air rockets of Germany]] |
||
[[Category:World War II weapons of Germany]] |
[[Category:World War II weapons of Germany]] |
Revision as of 01:28, 27 February 2019
This article needs additional citations for verification. (October 2013) |
R4M rocket | |
---|---|
Type | Rocket |
Place of origin | Germany |
Service history | |
In service | 1944-1945 |
Used by | Luftwaffe |
Wars | World War II |
Production history | |
Designed | 1944 |
Manufacturer | Heber AG, Osterode, Germany |
Variants | Air-to-air & Air-to-ground |
Specifications | |
Mass | 3.85 kg |
Length | 812 mm |
Width | 55 mm |
Muzzle velocity | 525 m/s (1,175 mph) |
Effective firing range | 600-1,000 m |
Maximum firing range | 1,500 m |
Filling weight | 520 g Hexogen for air-to-air role |
The R4M (Template:Lang-de) rocket, nicknamed the Hurricane (Template:Lang-de) due to its distinctive smoke trail when fired, was an anti-aircraft rocket. It was developed by the German Luftwaffe during World War II.
Development
The R4M was developed in order to deal with the increasing weight of anti-bomber weapons being deployed by Luftwaffe fighters. The primary anti-bomber weapon of the Luftwaffe for much of the war was the 20 mm MG 151/20 autocannon, which was compact enough to be mounted in an internal wing bay mounting in the Focke-Wulf Fw 190 (up to 4 cannon, or 6 with optional twin-gun underwing pods) and also fitted on the centerline of Bf 109G fighters, firing through the propeller spinner as a Motorkanone. This could be supplemented by an additional pair of cannon in drag-inducing underwing gun pods, but it was found that it took an average of twenty 20 mm hits to shoot down a typical four-engined Allied bomber. The MG 151/20 was subsequently supplemented with or replaced by the 30 mm MK 108 cannon, which replaced the centerline Motorkanone-mount MG 151/20 on many Bf 109's, and could be fitted into slightly larger underwing pods, which could be used on either the Bf 109 or Fw 190. This heavier-caliber cannon could bring down a bomber with an average of one to three hits. However the MK 108 was much heavier and the larger calibre ammunition made it difficult to carry more than one or two "passes" worth. Worse, the low muzzle velocity of this gun meant it had a very short range and suffered a ballistic drop of over 41 metres at 1,000 metres range after firing. In approaching close enough to get hits, the fighters placed themselves within the range of the dozens of AN/M2 "light barrel" Browning defensive machine guns that a combat box formation of a typical USAAF heavy bomber raid possessed, from nearly any approach direction. The more powerful MK 103 cannon had higher muzzle velocity and increased range, at the cost of greatly increased weight, size (barrel length of 1.34 meters, or 52-3/4 inches) and much lower rate of fire: 380-420 RPM vs. 600-650 RPM for the MK 108.
Also, the Nebelwerfer 42-derived Werfer-Granate 21 (Wfr. Gr. 21, or Bordrakete BR 21) rockets fitted to Messerschmitt Bf 109 and Bf 110, and Focke-Wulf Fw 190 fighters, used to break up the USAAF combat box bomber formations, had launch tubes that were not only drag-producing, due to their exposed five-strut under-wing mounting, but also from the fact that the launch tubes needed to be aimed upwards at some 15° from level flight, to counter the BR 21 rocket projectile's considerable ballistic drop after firing. This added to the already considerable drag the launch tube mountings created, and contributed to the Wfr. Gr 21's relatively slow projectile velocity of 1,150 km/h (715 mph), approximately 60% of the 505 m/s (1818 km/h) velocity of the MK 108 cannon's shells.
The solution was to replace the underwing gun pods, and the excessively drag-producing large-calibre underwing rocket launch tubes, with a small-diameter solid-fuel rocket-engine-propelled projectile, mounting a warhead similar to that of the cannon shell. Although each "round" was heavier than the corresponding gun-fired shell, the absence of a gun reduced the overall weight considerably. The weight difference was so great that even a much larger and longer-ranged rocket was still lighter than the guns it could replace, although the total number of rounds carried was also reduced from 65 rounds of 30 mm ammunition to only 24 rockets.
The anti-aircraft version of the R4M used a large warhead of 55 mm with 520 g. (17.6 ounces) of the strongly brisant Hexogen explosive charge, nearly guaranteeing a fighter kill with one hit, from the "shattering" force of its explosive warhead — this was the same explosive used in the shells fired by both the MK 103 (30 x 184 mm cartridge) and MK 108 (30 x 90 mm cartridge) autocannons. Each R4M weighed 3.2 kg and was provided with enough fuel to be fired from 1000 m, just outside the range of the bomber's defensive guns. The main body of the rocket consisted of a simple steel tube with eight base-hinged flip-out fins on the tail for stabilisation, deployed immediately after launch. A battery typically consisted of two groups of 12 rockets and when all 24 were salvoed in an attack, they would fill an area about 15 by 30 m at 1000 m, a density that made it almost certain that the target would be hit. The R4Ms were usually fired in four salvos of six missiles at intervals of 70 milliseconds from a range of 600 m, and would supersonically streak towards their target at a sixty percent higher velocity than the Wfr. Gr. 21's rockets would (the BR 21's projectile travelled at some 1150 km/h post-launch), as the R4M typically had a flight speed of roughly 1,890 km/h (1,175 mph). Two warheads were available for the R4M, the common PB-3 with a 0.4 kg charge for anti-aircraft use and the larger shaped charge, similar in construction to the Panzerschreck, the Panzerblitz (PB-2/3), for anti-tank use. The Panzerblitz III, mounting a gigantic 210 mm hollow charge warhead (the same calibre as the BR 21), can be seen as the ultimate development of the basic Orkan rocket. It was intended to be carried (six or eight rockets per plane) by the tank-busting B model of the Henschel Hs 132 jet dive-bomber - however, neither the missile nor the warplane it was exclusively intended for got beyond the prototype stage before the end of the war.
Operations
Only a small number of aircraft were fitted with the R4M, mostly Messerschmitt Me 262s and the ground attack version of the Fw 190s, which mounted them on small wooden racks under the wings. On one occasion, a Me 163A was fitted with several R4M rockets, and this setup was tested for several weeks in 1944, without incident. This was the first time a rocket propelled aircraft has had rocket propelled armament.
The Luftwaffe found the R4M missiles to have a similar trajectory to the 30 mm MK 108 cannon's rounds in flight, so the standard Revi 16B gunsight could be utilized.[1]
See also
- 3.5-inch FFAR rocket (US forces)
- 5-inch FFAR rocket (US forces)
- RP-3 (United Kingdom)
- RS-82 (rocket family) (Soviet Union)
References
- ^ Jeffrey L. Ethell; Alfred Price (1 April 1994). World War II fighting jets. Airlife. p. 38. ISBN 978-1-85310-406-0. Retrieved 3 September 2013.
- ^ Ziegler, Mano (July 1984). Rocket Fighter (2nd ed.). New York City: Bantam Books. pp. 155–156. ISBN 0-553-27348-5.
External links