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LGM-25C Titan II
Launch vehicle
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The Titan II was an intercontinental ballistic missile developed by the Glenn L. Martin Company from the earlier Titan I missile.
Wikipedia
Height
:
103.00 ft
Engine
:
Two-stage liquid-fueled rocket engines; first stage:
LR-87
; second stage:
LR91
Guidance system
:
Inertial
IBM
ASC-15
In service
:
1962 to 1987
Launch platform
:
Missile silo
Warhead
:
W-53
9 Mt thermonuclear warhead
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