Rheintochter

          The famous and versatile Rheinmetall-Borsig company developed the Rheintochter (Rhine Daughter) ground-to-air missile from 1942 onwards. The first experimental launching tests began in August 1943, and 82 had been fired and tested by 5 January 1945. Only four out of those 82 had failed. The propulsion mechanism included a motor driven by solid fuel, and a solid booster unit for initial take-off. Like the Schmetterling missile, the Rheintochter was guided through radio command and tracked visually by means of flare attached to the wings and fins. The warhead composed of 136kg of high explosive and was armed by a "Kranich" acoustic proximity fuze, like the X-4. The design altitude of the original Rheintochter was 8,000m, but the RLM rejected the design, requesting more altitude from the missile. The power system was then revised to employ solid or liquid fuels, and the booster rockets were placed outside the missile. It was also designed to be launched from an immovable launch site in a pit. This new version came to known as the Rheintochter 3, and production began in May 1944. Six had been built and fired by January 1945, but imperfection still plagued the control system. Development and thus production was canceled on 6 February 1945, as it became clear that the missile was not likely to be ready in time to have a significant impact on fate of the Reich.

Technical data and/or diagram of Rheintochter.
Rheintochter I ground-to-air missiles were based on solid-fuel.
A Rheintochter missile being tested, notice the flares fired to guide the ground controllers of the projectile's position.
An artist's drawing of the Rheintochter.

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