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  1. en.wikipedia.org › wiki › Atlas_IIAtlas II - Wikipedia

    Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. The Atlas II was a direct evolution of the Atlas I , featuring longer first-stage tanks, higher-performing engines, and the option for strap-on solid rocket boosters.

  2. May 10, 2024 · Used by Devlin Stone, this Atlas variant used a combination of Clan and Inner Sphere technology to maximize survival. The ER large lasers, XL engine, and heat sinks came from Clan sources. A heavy-duty gyro is also fitted to enhance survivability.

  3. The Atlas-Centaur was evolved into the Atlas II, various models of which were launched 63 times between 1991 and 2004. There were only six launches of the succeeding Atlas III, all between 2000 and 2005. The Atlas V is still in service, with launches planned into the mid 2020s.

    Model Name
    First Launch
    Last Launch
    Total Launches
    1959
    1960
    3
    Atlas LV-3A
    1960
    1968
    49
    1959
    1963
    9
    1964
    1968
    51
  4. www.wikiwand.com › en › Atlas_IIAtlas II - Wikiwand

    The Atlas II was a direct evolution of the Atlas I, featuring longer first stage tanks, higher-performing engines, and the option for strap-on solid rocket boosters. It was designed to launch payloads into low Earth orbit, geosynchronous transfer orbit or geosynchronous orbit.

  5. First Launch: 1991-12-07. Last Launch: 1998-03-16. Number: 10 . Payload: 6,580 kg (14,500 lb). Thrust: 2,110.60 kN (474,482 lbf). Gross mass: 187,600 kg (413,500 lb). Height: 47.50 m (155.80 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi). LEO Payload: 6,580 kg (14,500 lb) to a 185 km orbit at 28.50 degrees.

  6. Atlas II. Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit, or geosynchronous orbit. The Vernier engines on the first stage of the Atlas I were replaced by a hydrazine fueled ...

  7. Atlas II was a member of the Atlas family of launch vehicles, which evolved from the successful Atlas missile program of the 1950s. It was designed to launch payloads into low earth orbit, geosynchronous transfer orbit or geosynchronous orbit. Sixty-three launches of the Atlas II, IIA and IIAS models were carried out between 1991 and 2004; all ...

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