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MSBS M2
Part of MSBS Family
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: S610. LV Family: MSBS. Launch Vehicle: MSBS M2.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 600 km (370 mi).

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 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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