. . . . "1"^^ . . . "O Delta C foi um foguete dos estadunidense que prestou servi\u00E7o entre 1963 e 1967."@pt . "1969-01-22"^^ . "Thor Delta C \u2013 ameryka\u0144ska rakieta no\u015Bna z rodziny . Istnia\u0142y jej dwa warianty: C (10 start\u00F3w) i C1 (3 starty)."@pl . "Retired" . "\u0414\u0435\u043B\u044C\u0442\u0430-C"@ru . "Delta C"@pt . . . "Thor Delta C"@pl . . . "1969-01-22"^^ . . . . . . . "2161"^^ . "United States"@en . "21471235"^^ . . . "\u00AB\u0414\u0435\u043B\u044C\u0442\u0430-C\u00BB \u2014 \u0430\u043C\u0435\u0440\u0438\u043A\u0430\u043D\u0441\u043A\u0430\u044F \u0440\u0430\u043A\u0435\u0442\u0430-\u043D\u043E\u0441\u0438\u0442\u0435\u043B\u044C \u043B\u0451\u0433\u043A\u043E\u0433\u043E \u043A\u043B\u0430\u0441\u0441\u0430, \u0441\u0435\u043C\u0435\u0439\u0441\u0442\u0432\u0430 \u0414\u0435\u043B\u044C\u0442\u0430."@ru . . . . "Retired"@en . . . "12"^^ . . . . . . "13"^^ . . . . . . . . "1963-11-27"^^ . . . "12"^^ . . . . "\u00AB\u0414\u0435\u043B\u044C\u0442\u0430-C\u00BB \u2014 \u0430\u043C\u0435\u0440\u0438\u043A\u0430\u043D\u0441\u043A\u0430\u044F \u0440\u0430\u043A\u0435\u0442\u0430-\u043D\u043E\u0441\u0438\u0442\u0435\u043B\u044C \u043B\u0451\u0433\u043A\u043E\u0433\u043E \u043A\u043B\u0430\u0441\u0441\u0430, \u0441\u0435\u043C\u0435\u0439\u0441\u0442\u0432\u0430 \u0414\u0435\u043B\u044C\u0442\u0430."@ru . . . "1"^^ . . "O Delta C foi um foguete dos estadunidense que prestou servi\u00E7o entre 1963 e 1967."@pt . "Delta C"@en . "1963-11-27"^^ . "The Delta C, or Thor-Delta C was an American expendable launch system used for thirteen orbital launches between 1963 and 1969. It was a member of the Delta family of rockets. The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the , which was derived from the earlier . The baseline Delta C used an Altair-2 third stage, whilst the Delta C1 had an third stage, which provided a higher payload capacity than the Altair. It is unclear whether two or three launches were made using the C1 configuration. The Delta C was launched from Cape Canaveral Air Force Station Launch Complex 17. Most launches carried NASA research satellites into low Earth orbit."@en . . . . . . "1084018898"^^ . . "Thor Delta C \u2013 ameryka\u0144ska rakieta no\u015Bna z rodziny . Istnia\u0142y jej dwa warianty: C (10 start\u00F3w) i C1 (3 starty)."@pl . "The first Delta C launches with Explorer 18"@en . . "180"^^ . . . . "The Delta C, or Thor-Delta C was an American expendable launch system used for thirteen orbital launches between 1963 and 1969. It was a member of the Delta family of rockets. The first stage was a Thor missile in the DSV-2A configuration, and the second stage was the , which was derived from the earlier . The baseline Delta C used an Altair-2 third stage, whilst the Delta C1 had an third stage, which provided a higher payload capacity than the Altair. It is unclear whether two or three launches were made using the C1 configuration."@en . . . "13"^^ .