SM-68B Titan II

SM-68B Titan II
Ilustracja
Państwo Stany Zjednoczone
ProducentMartin Marietta
Inne nazwyLGM-25C
TypICBM
Przeznaczeniepocisk strategiczny
Wyrzutniasilosy, wyrzutnie naziemne
Statuszdezaktywowany
Lata służby1963-1987
Długość31,30 m
Średnica3,05 m
Masa startowa149 700 kg
Napęd2 silniki LR-87 w 1. stopniu, w drugim 1 LR-91
Zasięg15 000 km
Udźwigpojedyncza głowica
Naprowadzaniebezwładnościowe z komputerem cyfrowym
CelnośćCEP: 900 m
GłowicaW-53/Mk-6 jądrowa o mocy 9Mt

SM-68B Titan IIamerykański dwustopniowy rakietowy pocisk balistyczny o zasięgu międzykontynentalnym (ICBM) na paliwo ciekłe. Pozostające na wyposażeniu Sił Powietrznych Stanów Zjednoczonych w latach 1963–1987 pociski Titan II, zaprojektowane były do przenoszenia jednej głowicy jądrowej W-53/Mk-6 o mocy 9 megaton.

Linki zewnętrzne

  • SM-68B Titan II (ang.). W: Weapons of Mass Destruction [on-line]. Federation of American Scientists, 1997. [dostęp 2017-06-23].
  • Mark Wade: Titan II (ang.). W: Encyclopedia Astronautica [on-line]. [dostęp 2017-06-23].

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Gemini-Titan 11 Launch - GPN-2000-001020.jpg
Lift-off of Gemini-Titan 11 (GT-11) on Complex 19. The Gemini 11 mission included a rendezvous with an Agena target vehicle.
Titan IVB launching Lacrosse satellite.jpg
Team Vandenberg launched a Titan IV-B rocket from Space Launch Complex 4 East on August 17, 2000. The rocket carried a National Reconnaissance Office satellite into orbit. "The 30th Space Wing, Space and Missile Center, NRO and Lockheed Martin Aerospace have worked together to build upon our legacy of success," said Col. Steve Lanning, 30th Space Wing commander and spacelift commander for the mission. "This marks the 1,800th launch from Vandenberg. We have built a solid foundation for government and commercial space launches from here for years to come." Payload-booster separation successfully occurred at 4:54.15 p.m.
Titan2 color silo.jpg
A U.S. Air Force LGM-25C Titan II ICBM undergoes a test launch from an underground silo. Unlike Titan I missiles, which had to be raised to the surface before launch, the Titan II’s liquid rocket engines were ignited while it was still in the silo. Therefore the silo had to be constructed with flame and exhaust ducts as shown in this photograph.