SSBS S1
Function | Experimental medium-range ballistic missile |
---|---|
Manufacturer | SEREB |
Country of origin | France |
Cost per year | 1965–1993 |
Size | |
Height | 15.10 metres (49.5 ft) |
Diameter | 1.50 metres (59 in) |
Mass | 25,000 kilograms (55,000 lb) |
Capacity | |
Payload to {{{to}}} | |
Launch history | |
Status | Retired |
Total launches | 53 |
Success(es) | 53 |
Failure(s) | 0 |
Partial failure(s) | 0 |
First flight | 23 October 1965 |
Last flight | 3 November 1993 |
stage | |
Powered by | S1 LRE liquid |
Maximum thrust | 440 kilonewtons (99,000 lbf) |
Propellant | LOX / UDMH |
[edit on Wikidata] |
The SSBS was a series of French military medium-range ballistic missiles.
Overview
The first series, SSBS S1, was launched between 1965 and 1968. It had a maximum altitude of 500 kilometres (310 mi), a lift off thrust of 440 kN, total mass of 25,000 kilograms (55,000 lb), a diameter of 1.50 metres (59 in) and a total length of 15.10 metres (49.5 ft).[1]
References
- ^ "SSBS". Encyclopedia Astronautica. Archived from the original on December 6, 2007.
- v
- t
- e
French nuclear armament
- missile M1
- missile M2
- missile M20
- missile S1
- missile S2
- missile S3
- missile M4
- missile M45
- missile M5
- missile M51
- French nuclear deterrence
- FAS
- FOST
- France and weapons of mass destruction
This rocketry article is a stub. You can help Wikipedia by expanding it. |
- v
- t
- e