SM-68B Titan II
| Length | 103 ft. / 31.7 meters(ICBM configuration) |
| First stage length | 70 ft. |
| Diameter | 10 ft. (first & second stages - ICBM configuration). |
| Weight | 270,000 lbs. at launch |
| Armament | 1 x General Electric Mk. 6 Nuclear warhead |
| Engines: First stage | Aerojet LR87-AJ-5 two chamber liquid propellant rocket of 430,000 lbs. thrust fueled by Aerozine-50 (fuel) that ignites on contact with nitrogen tetroxide (oxidizer). |
| Second stage | Aerojet-General LR91-AJ-5 rocket engine of 100,000 lbs. Thrust |
| Maximum speed | 15,000 mph / 13,904 knots |
| Maximum range | Approximately 10,000 statute miles / 8,700 nautical miles |
| Maximum altitude | 700 statute miles / 610 nautical miles |
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