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MBB design for a vertical-launch, horizontal landing two-stage winged launch vehicle. The upper stage had a configuration similar to the later US shuttle, with a seventy-degree double-delta wing, except with wingtip fins as on Dyna-Soar. The design effort was funded from 1962-1969 with DM 16.5 million of German government funds. Crew Size: 2. Bibliography:
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