Alfa (rocket): Difference between revisions
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'''Alfa''' was the designation of an Italian [[solid propellant]] [[intermediate-range ballistic missile]] program that started in 1971 under the control of the GRS (Gruppo di Realizzazione Speciale Interforze). Starting as a development effort for a study on efficient solid-propellant rockets, the Alfa rocket was planned as a two-stage rocket. Test launches with an upper stage mockup took place between 1973 and 1975, from [[Salto di Quirra]]. |
'''Alfa''' was the designation of an Italian [[solid propellant]] [[intermediate-range ballistic missile]] program that started in 1971 under the control of the GRS (Gruppo di Realizzazione Speciale Interforze). Starting as a development effort for a study on efficient solid-propellant rockets, the Alfa rocket was planned as a two-stage rocket. Test launches with an upper stage mockup took place between 1973 and 1975, from [[Salto di Quirra]]. |
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The Alfa was {{convert|6.5|m}} long and had a diameter of {{convert|1.37|m}}. The first stage of the Alfa was {{convert|3.85|m}} long and contained 6 t of solid rocket fuel. It supplied a thrust of 232 [[Newton (unit)|kN]] for a duration of 57 seconds. |
The Alfa was {{convert|6.5|m}} long and had a diameter of {{convert|1.37|m}}. The first stage of the Alfa was {{convert|3.85|m}} long and contained 6 t of solid rocket fuel. It supplied a thrust of 232 [[Newton (unit)|kN]] for a duration of 57 seconds. |
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Revision as of 09:42, 22 August 2017
 | This article needs additional citations for verification. (October 2013) |
| Alfa | |
|---|---|
 Test launch of an Alfa | |
| Type | Intermediate range ballistic missile |
| Place of origin | Italy |
| Service history | |
| In service | 1973-1976 |
| Used by | Italian Navy |
| Production history | |
| Manufacturer | Aeritalia, Selenia, Snia BPD |
| No. built | 6 |
| Specifications | |
| Mass | 8,000 kilograms (18,000 lb) |
| Length | 3.85 metres (12.6 ft) |
| length | first stage |
| Height | 6.5 metres (21 ft) |
| Diameter | 1.37 metres (54 in) |
| Warhead | Nuclear warhead |
| Engine | first stage, solid fuel rocket 250 kN (56,000 lbf) thrust second stage, solid fuel rocket thrust unknown |
Operational range | 1,600 kilometres (990 mi) with 1 Mt warhead |
| Flight altitude | apogee 300 km (190 mi) |
| Boost time | first stage, 57 seconds second stage, unknown |
Guidance system | Inertial |
Launch platform | surface vessels |
Alfa was the designation of an Italian solid propellant intermediate-range ballistic missile program that started in 1971 under the control of the GRS (Gruppo di Realizzazione Speciale Interforze). Starting as a development effort for a study on efficient solid-propellant rockets, the Alfa rocket was planned as a two-stage rocket. Test launches with an upper stage mockup took place between 1973 and 1975, from Salto di Quirra.
The Alfa was 6.5 metres (21 ft) long and had a diameter of 1.37 metres (4 ft 6 in). The first stage of the Alfa was 3.85 metres (12.6 ft) long and contained 6 t of solid rocket fuel. It supplied a thrust of 232 kN for a duration of 57 seconds.
It was capable of carrying a warhead of 1 Mt and had a range of 1,600 kilometres (990 mi), which meant that it could reach all eastern countries and the western USSR if launched from frigates or destroyers in the Adriatic Sea.[1] Italy has been active in the space sector since 1957, conducting launch and control operations from the Luigi Broglio Space Centre. The advanced Scout and Vega launchers currently used by the European Space Agency (ESA) derive their technological basis partially from Alfa studies.[1]
An Alfa rocket is currently displayed at the Cameri Air Base Museum in Novara Province.
References
External links
- "Alfa". Encyclopedia Astronautica. Retrieved 6 October 2013.
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