RSD 58: Difference between revisions
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Design work on the RSD-58 commenced in 1947, resulting in a liquid-fuelled rocket powered missile guided to its target by riding a radar beam. The complete system includes a battery command post, target tracking radar, guidance beam transmitter and six twin railed trainable launchers. The entire system including the static launchers is readily transported to new locations with mobility claimed to be similar to that of a heavy [[anti-aircraft gun]] system.<ref name=JAWA62-63/> |
Design work on the RSD-58 commenced in 1947, resulting in a liquid-fuelled rocket powered missile guided to its target by riding a radar beam. The complete system includes a battery command post, target tracking radar, guidance beam transmitter and six twin railed trainable launchers. The entire system including the static launchers is readily transported to new locations with mobility claimed to be similar to that of a heavy [[anti-aircraft gun]] system.<ref name=JAWA62-63/> |
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Test firings commenced in Switzerland during 1950-51, with a batch of 25 pre-production missiles being evaluated at [[Holloman air force base]] in [[New Mexico]] [[USA]] in 1953. |
Test firings commenced in Switzerland during 1950-51, with a batch of 25 pre-production missiles being evaluated at [[Holloman air force base]] in [[New Mexico]] [[USA]] in 1953. |
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Targetting is by search radar and beam transmitter with targets tracked by a search radar until a beam riding transmitter locks on, at which point the missile can be fired, riding the beam until impact, proximity fuze or radio signal detonation. Launchers, slaved to the beam transmitter can launch missiles at any angle form 10° to 90°. Control of the missiles is by vectoring rocket motor combustion chamber at low speeds and controllable rear fins at higher speeds.<ref name=JAWA62-63/> |
Targetting is by search radar and beam transmitter with targets tracked by a search radar until a beam riding transmitter locks on, at which point the missile can be fired, riding the beam until impact, proximity fuze or radio signal detonation. Launchers, slaved to the beam transmitter can launch missiles at any angle form 10° to 90°. Control of the missiles is by vectoring rocket motor combustion chamber at low speeds and controllable rear fins at higher speeds.<ref name=JAWA62-63/> |
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Revision as of 17:00, 1 May 2013
Missile system RSC / D
| RSC/D | |
|---|---|
 RSC/D Missile on dupplex fireingcarrier at Militärmuseum Full | |
| Type | Surface-to-air missile |
| Place of origin |  Switzerland |
| Service history | |
| In service | 1960–? |
| Used by | Japan |
| Production history | |
| Designed | 1958 |
| Manufacturer | Oerlikon Contraves |
| Produced | 1958-1960 |
| Specifications | |
| Mass | missile:400kg, Carrierwagon: 4700kg, Comunication/steering wagon:5500kg |
| Warhead | 40kg warhead |
| Engine | nitride acid / kerosene mixture |
Operational range | 30000 m |
| Flight ceiling | 9,000 m |
| Maximum speed | Mach 2.4 (800m/s) |
Guidance system | Beamcontrol |
Steering system | control surface |
Launch platform | vehicle or trailer |
- Operation = 9: 1 operator, 8 Charging team
The missile system RSC / D of the company Oerlikon Contraves was built in 1958 and tested in Italy.
The RSD 58 is an early production surface-to-air missile system developed by Contraves Oerlikon in Switzerland from 1947. Test firings were first made in 1950 with production starting in 1952 for the armed forces of Japan[1], testshots are made in Switzerland and Italy. On the basis of the missile RSA, the beacon controlled missile system RSC / D was developed. There was no significant order, except for the delivery of a training battery to Japan and thus no larger order. The system consists of double start carriage, beacon, search radar, command station and diesel generator. All five components are each constructed on a single-axle trailer apart from the diesel generator that was built on a two-axle trailer. The two hydraulic elevierbaren bars throw on / trolley enabled a self-assemble with rocket was thus no additional crane / loading vehicle necessary. The system RSC / D in 1960 was the basis of the developed under the code names Kriens RSD system, which was completed in 1966 by EMD. The Air Force used instead, the British Bloodhound system. A double carriage start of the RSC / D with 2 missiles and a beacon is now at the Full Military Museum. Start a double mount with 2 missile system RSD Kriens is now at the Aviation Museum in Dübendorf.
Design and development
Design work on the RSD-58 commenced in 1947, resulting in a liquid-fuelled rocket powered missile guided to its target by riding a radar beam. The complete system includes a battery command post, target tracking radar, guidance beam transmitter and six twin railed trainable launchers. The entire system including the static launchers is readily transported to new locations with mobility claimed to be similar to that of a heavy anti-aircraft gun system.[1]
Test firings commenced in Switzerland during 1950-51, with a batch of 25 pre-production missiles being evaluated at Holloman air force base in New Mexico USA in 1953.
Targetting is by search radar and beam transmitter with targets tracked by a search radar until a beam riding transmitter locks on, at which point the missile can be fired, riding the beam until impact, proximity fuze or radio signal detonation. Launchers, slaved to the beam transmitter can launch missiles at any angle form 10° to 90°. Control of the missiles is by vectoring rocket motor combustion chamber at low speeds and controllable rear fins at higher speeds.[1]
A parachute recoverable training round, the RSC-57, has been developed which is powered by a reduced burn time rocket motor with the recovery parachute replacing the warhead.[1]
Operational history
This missile system has seen active service in Switzerland, Italy and Japan.[1]
References
- Hugo Schneider: armament and equipment of the Swiss Army since 1817: light and medium anti-aircraft air defence anti-aircraft missiles, Volume 12 of armament and equipment of the Swiss Army since 1817, Author Publisher Stocker-Schmidt, 1982
Notes
Bibliography
- Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.
- Hogg, Ian: Tykistö- ja ohjusaseet, Karisto, 2011, Hämeenlinna (Translated by: Petri Kortesuo) ISBN 978-951-23-5456-6 (s.209)