Reading level:
A kid-friendly version of this page isn’t written yet — you’re seeing the regular version below. Back to the gallery to find an aircraft with a Kids version.

Martin Marietta Titan (missile)

Martin Marietta · Ballistic · USA · Early Jet (1946–1969)

Martin Marietta Titan (missile) — Ballistic
Open in interactive gallery →

The Titan II was an intercontinental ballistic missile (ICBM) developed by the Glenn L. Martin Company from the earlier Titan I missile. Titan II was originally designed and used as an ICBM, but was later adapted as a medium-lift space launch vehicle to carry payloads to Earth orbit for the United States Air Force (USAF), National Aeronautics and Space Administration (NASA) and National Oceanic and Atmospheric Administration (NOAA). Those payloads included the USAF Defense Meteorological Satellite Program (DMSP), NOAA weather satellites, and NASA's Gemini crewed space capsules. The modified Titan II SLVs were launched from Vandenberg Air Force Base, California, up until 2003.

Specifications

Category
Missiles
Sub-Category
Ballistic
Domain
Defence
Era
Early Jet (1946–1969)
Country
USA
Manufacturer
Martin Marietta
Operator
USA
Primary Role
Ballistic
Status
Retired
Service Entry
1963
Produced
54
Engine
Aerojet LR87/LR91 liquid (N2O4/Aerozine-50) 2-stage
Thrust / Power
430,000 lbf
Launch
Silo-launched
Length (ft)
103
MTOW (lb)
330000
Payload (lb)
8000
Service Ceiling (ft)
900000
Range (mi)
9300
Max Speed (mph)
17641
Max Speed (Mach)
23
Armament
Nuclear W53 9 Mt