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.

Most Titan rockets were the Titan II, which could carry a W-53 nuclear warhead with a nine megaton yield, making it the most powerful ICBM on-standby in the US nuclear arsenal. These were deployed in three squadrons of 18 missiles each, in Arizona, Kansas, and Arkansas. All of the ICBM Titan II missile sites have been decommissioned since the retirement of the Titan II as an ICBM in 1987, but the Titan Missile Museum on Interstate 19 south of Tucson, Arizona, has preserved one deactivated launch site. The Titan II was a two-stage ICBM that was used by the US Air Force from the mid-1960s to the mid-1980s. The Titan II used a hypergolic combination of nitrogen tetroxide and hydrazine for propellant. In addition to its use as an ICBM, twelve Titan II missiles were converted to launch Gemini spacecraft for NASA, ten of which were manned. Following retirement, a further thirteen were converted to the Titan 23G configuration, and used to launch satellites, and the Clementine Lunar probe. The last Titan II launch occurred in 2003.

From : Wikipedia

GENERAL INFO

  • Created On: Android
  • Game Version: 0.9.700.0
  • Price: $8,964k
  • Number of Parts: 318
  • Dimensions: 30 m x 3 m x 3 m

PERFORMANCE

  • Total Delta V: 4.0km/s
  • Total Thrust: 2.2MN
  • Engines: 5
  • Wet Mass: 87,267kg
  • Dry Mass: -13,530kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 4 2.5km/s 1.8MN 82s 87,267kg
2 1 1.5km/s 433kN 77s 28,607kg

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