Rheintochter

Rheintochter was a German surface-to-air missile developed during World War II.

History

Rheintochter was ordered in November 1942 by the German army. Starting in August 1943, 82 test firings were made. An air-launched version was also designed. The project was cancelled in February 6, 1945.

Variants

The initial R1 variant was powered by 2 stages solid fuel rockets. Because this lacked the ability to reach high altitudes, the R3 model was developed, which had a liquid fuel motor with solid-fuel boosters

Characteristics

  • Primary Function: surface-to-air missile
  • Contractor: Rheinmetall-Borsig
  • Power Plant: RI variant was 2-stage solid fuel; RIII was liquid fuel with solid-fuel boosters
  • Length: 10.3 m
  • Diameter: cm
  • Wing Span: cm
  • Launch Weight: kg
  • Speed:
  • Warhead: 136 kg explosive
  • Range: km
  • Altitude: R1 8 km
  • Fuzes: "Kranich" acoustic proximity fuze
  • Guidance system: MCLOS visual guidance. The rocket had flares located on the wingtips to help the operator keep track of it.
  • Unit Cost:
  • Date Deployed:
  • Users: Germany

See also

 

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