SM-68 Titan

http://dbpedia.org/resource/SM-68_Titan an entity of type: Thing

SM-68 Titan (varian individu kemudian ditunjuk HGM-25 dan LGM-25) adalah sebutan untuk dua rudal balistik antarbenua Amerika, yang merupakan anggota keluarga dari roket Titan. Ini terdiri dari rudal Titan I dan Titan II, yang beroperasi antara tahun 1962 dan 1987, dan merupakan komponen utama dari armada rudal Amerika Serikat selama Perang Dingin. rdf:langString

The SM-68 Titan (individual variants later designated HGM-25 Titan I and LGM-25 Titan II) was the designation of two intercontinental ballistic missiles developed for the United States Air Force. The Titan I and Titan II missiles were operational between 1962 and 1987 during the Cold War. These missiles, particularly the Titan II, were the basis of the Titan family of space launch vehicles. rdf:langString

O SM-68 Titan, foi a designação original de um ICBM de origem Norte americana. O significado das letras SM, vem do termo em inglês Strategic Missile. Os mísseis desse modelo estiveram ativos entre 1962 e 1987, fazendo parte de frota de mísseis dos Estados Unidos durante a "Guerra Fria". O SM-68 Titan fazia parte da família de foguetes Titan. Ele foi originalmente construído como uma alternativa para o míssil SM-65 Atlas, caso o projeto daquele sofresse algum atraso. Para esse míssil, foram desenvolvidas duas versões, cada uma usando uma combinação de propelentes diferente: rdf:langString

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rdf:langString SM-68 Titan

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xsd:integer 20052024

dbpedia-owl:wikiPageRevisionID

xsd:integer 1084023154

dbpedia-owl:abstract

rdf:langString SM-68 Titan (varian individu kemudian ditunjuk HGM-25 dan LGM-25) adalah sebutan untuk dua rudal balistik antarbenua Amerika, yang merupakan anggota keluarga dari roket Titan. Ini terdiri dari rudal Titan I dan Titan II, yang beroperasi antara tahun 1962 dan 1987, dan merupakan komponen utama dari armada rudal Amerika Serikat selama Perang Dingin. Titan awalnya dibangun sebagai cadangan untuk SM-65 Atlas. Titan I menggunakan RP-1 dan propelan oksigen cair, sehingga waktu respon sekitar lima belas menit, diperlukan untuk bahan bakar roket dan meningkatkan ke posisi peluncuran. Ia digantikan oleh Titan II yang lebih kuat, yang menggunakan nitrogen ferri dan hidrazin, memungkinkan untuk disimpan dengan propelan dimuat, memberikan waktu respon lebih pendek.

rdf:langString The SM-68 Titan (individual variants later designated HGM-25 Titan I and LGM-25 Titan II) was the designation of two intercontinental ballistic missiles developed for the United States Air Force. The Titan I and Titan II missiles were operational between 1962 and 1987 during the Cold War. These missiles, particularly the Titan II, were the basis of the Titan family of space launch vehicles. Titan was originally built as a backup to the SM-65 Atlas. The Titan I used RP-1 and liquid oxygen propellants and required around fifteen minutes to load the rocket and raise it to a launch position. The more powerful Titan II used nitrogen tetroxide and hydrazine, allowing it to be stored with propellant loaded, giving it a much shorter response time.

rdf:langString O SM-68 Titan, foi a designação original de um ICBM de origem Norte americana. O significado das letras SM, vem do termo em inglês Strategic Missile. Os mísseis desse modelo estiveram ativos entre 1962 e 1987, fazendo parte de frota de mísseis dos Estados Unidos durante a "Guerra Fria". O SM-68 Titan fazia parte da família de foguetes Titan. Ele foi originalmente construído como uma alternativa para o míssil SM-65 Atlas, caso o projeto daquele sofresse algum atraso. Para esse míssil, foram desenvolvidas duas versões, cada uma usando uma combinação de propelentes diferente: * A primeira foi a HGM-25A Titan I * A segunda foi a LGM-25C Titan II

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