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  2. Titan (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Titan_(rocket_family)

    Titan was a family of United States expendable rockets used between 1959 and 2005. The Titan I and Titan II were part of the US Air Force's intercontinental ballistic missile (ICBM) fleet until 1987. The space launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed

  3. List of Titan launches - Wikipedia

    en.wikipedia.org/wiki/List_of_Titan_launches

    Rockets from the Titan family accumulated 368 launches between 1959 and 2005, 322 of which were successful, yielding a 87.5% success rate. 5. 10. 15. 20. 25. 30. 1959 ...

  4. Titan IIIE - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIE

    The Titan IIIE or Titan 3E, also known as the Titan III-Centaur, was an American expendable launch system. Launched seven times between 1974 and 1977, [ 4 ] it enabled several high-profile NASA missions, including the Voyager and Viking planetary probes and the joint West Germany-U.S. Helios spacecraft .

  5. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    All launch vehicle propulsion systems employed to date have been chemical rockets falling into one of three main categories: Solid-propellant rockets or solid-fuel rockets have a motor that uses solid propellants, typically a mix of powdered fuel and oxidizer held together by a polymer binder and molded into the shape of a hollow cylinder. The ...

  6. Category:Titan (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Category:Titan_(rocket_family)

    Pages in category "Titan (rocket family)" The following 17 pages are in this category, out of 17 total. This list may not reflect recent changes. ...

  7. Titan IIIC - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIC

    The Titan III family consisted of an enhanced Titan II core with or without solid rocket strap-on boosters and an assortment of upper stages. All Solid Rocket Motor (SRM)-equipped Titans (IIIC, IIID, IIIE, 34D, and IV) launched with only the SRMs firing at liftoff, the core stage not activating until T+105 seconds, shortly before SRM jettison.

  8. Titan II GLV - Wikipedia

    en.wikipedia.org/wiki/Titan_II_GLV

    The Titan II was a two-stage liquid-fuel rocket, using a hypergolic propellant combination of Aerozine 50 fuel and nitrogen tetroxide oxidizer. The first stage was powered by an LR87 engine (with two combustion chambers and nozzles, fed by separate sets of turbomachinery), [ 2 ] [ 3 ] and the second stage was propelled by an LR-91 engine.

  9. List of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/List_of_orbital_launch_systems

    Comparison of Saturn V, Space Shuttle, three Ares rockets, and SLS Block 1 Titan rockets. Ares – Canceled. Ares I; Ares IV; Ares V; Astra Space launch vehicles. Rocket 3 – Retired; Rocket 4 – Under development; Athena – Retired. Athena I; Athena II; Atlas. Atlas B – Retired; Atlas D – Retired; Atlas-Able – Retired; Atlas-Agena ...