"0"^^ . . "Saturn II"@en . "10.0584"^^ . "2"^^ . "3.28406e+08"^^ . . . "50.9016"^^ . . . "The Saturn II was a series of proposed American Expendable launch vehicles, proposed by North American Aviation in 1966, derived from the Saturn V rocket that was used for the Apollo lunar program. It was, essentially, a version of the Saturn V with the lowest stage removed, producing a two-stage design with a payload intermediate between the Saturn IB and V, delivering about 46,000 pounds (21,000 kg) to low earth orbit."@en . . . "2.13192e+07"^^ . "Cancelled" . "1967 Study" .