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MSBS M2
Part of MSBS
French intermediate range ballistic missile. Two stage vehicle consisting of 1 x SEP 904 + 1 x Rita II
Status: Retired 1973. First Launch: 1973-01-01. Last Launch: 1973-07-20. Number: 3 . Payload: 1,360 kg (2,990 lb). Thrust: 440.00 kN (98,910 lbf). Gross mass: 19,500 kg (42,900 lb). Height: 10.67 m (35.00 ft). Diameter: 1.52 m (4.98 ft). Span: 1.52 m (4.98 ft). Apogee: 600 km (370 mi).
Maximum range: 3,200 km (1,900 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1973.
Subtopics
| SEP 904 Sud/SEP solid rocket engine. MSBS M2 first stage. |
| Rita II Sud/SEP solid rocket engine. MSBS M2 second stage. |
Family:
IRBM,
submarine-launched.
Country:
France.
Launch Sites:
Biscarosse,
Biscarosse BLB.
Stages:
SEP 904,
Rita II.
Agency:
SEREB.
1973 - .
Launch Site:
Biscarosse.
Launch Platform: S655.
LV Family:
MSBS.
Launch Vehicle:
MSBS M2.
- Operational test - .
Nation: France.
Agency: DMA.
Apogee: 600 km (370 mi).
1973? - .
Launch Site:
Biscarosse.
Launch Platform: S610.
LV Family:
MSBS.
Launch Vehicle:
MSBS M2.
- Operational test - .
Nation: France.
Agency: DMA.
Apogee: 600 km (370 mi).
1973 July 20 - .
Launch Site:
Biscarosse.
Launch Complex:
Biscarosse BLB.
LV Family:
MSBS.
Launch Vehicle:
MSBS M2.
- Operational test - .
Nation: France.
Agency: DMA.
Apogee: 600 km (370 mi).
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