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  2. Solid Rocket Motor Upgrade - Wikipedia

    en.wikipedia.org/wiki/Solid_Rocket_Motor_Upgrade

    The Solid Rocket Motor Upgrade (SRMU) was a solid rocket motor that was used as a booster on the Titan IVB launch vehicle. Developed by Hercules (later ATK), it was intended to be a high-performance, low-cost upgrade to the UA1207 boosters previously used on Titan IV.

  3. Titan (rocket family) - Wikipedia

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

    Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA.The Titan II used the LR-87-5 engine, a modified version of the LR-87, that used a hypergolic propellant combination of nitrogen tetroxide (NTO) for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and unsymmetrical dimethylhydrazine (UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I.

  4. List of Titan launches - Wikipedia

    en.wikipedia.org/wiki/List_of_Titan_launches

    First Gemini launch, first orbital Titan launch 9 April 20:00 Titan II: N-3A CCAFS LC-15: Suborbital: Success 30 July Titan II: B-28 VAFB LC-395-D: Suborbital: Success "Cobra Skin" [3] 11 August Titan II: B-9 VAFB LC-395-D: Suborbital: Success "Double Talley" [3] 13 August Titan II: B-7 VAFB LC-395-D: Suborbital: Success "Gentle Annie" [3] 1 ...

  5. Titan IIIC - Wikipedia

    en.wikipedia.org/wiki/Titan_IIIC

    The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly.

  6. Opinion - The NASA-SpaceX launch to Titan sparks dreams of ...

    www.aol.com/opinion-nasa-spacex-launch-titan...

    Recently, NASA selected the SpaceX Falcon Heavy to launch the Dragonfly aerial probe to Titan, Saturn’s largest moon. The selection constitutes another win for Elon Musk’s launch company.

  7. Aerojet LR87 - Wikipedia

    en.wikipedia.org/wiki/Aerojet_LR87

    Used on the Titan I, the LR87-3 burned liquid oxygen and RP-1. [4] Following the retirement of the Titan missile program, these engines saw no further use. [citation needed] The LR87-3 was also operated with NTO/Aerozine 50 and ground tested with LOX/H2 (with a new fuel pump), making it one of very few engines to have been run on three different propellant combinations.

  8. Titan 23G - Wikipedia

    en.wikipedia.org/wiki/Titan_23G

    The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American expendable launch system derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta , into which the Glenn L. Martin Company , which built the original Titan II, had merged.

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