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  1. Atlas-Centaur AC-27 at Launch Complex 36A in February 1972 prior to launching Pioneer 10. Initially, a modified Atlas D designated LV-3C was used as the first stage. This was quickly replaced by SLV-3C, and later the SLV-3D, both derived from the standard Atlas SLV-3 rocket.

  2. en.wikipedia.org › wiki › Atlas-AgenaAtlas-Agena - Wikipedia

    The Atlas-Agena was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was launched 109 times between 1960 and 1978. [1] It was used to launch the first five Mariner uncrewed probes to the planets Venus and Mars , and the Ranger and Lunar Orbiter uncrewed probes to the ...

    • 26 February 1960
    • 109
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  4. Variants. SM-65 Atlas. SM-65D Atlas. Atlas LV-3C. Atlas IIIA. Atlas V. Atlas is a family of US missiles and space launch vehicles that originated with the SM-65 Atlas. The Atlas intercontinental ballistic missile (ICBM) program was initiated in the late 1950s under the Convair Division of General Dynamics. [2]

    • December 17, 1957; 65 years ago
    • 1957–2010s (decade)
  5. Atlas LV-3C s/n AC-3 / Centaur D s/n 135D - 1964-06-30. American orbital launch vehicle. Version with basic Centaur upper stage. AKA: LV-3C. Payload: 1,700 kg (3,700 lb). Thrust: 173,843.00 kN (39,081,461 lbf). Gross mass: 136,124 kg (300,102 lb). Height: 33.00 m (108.00 ft). Diameter: 3.05 m (10.00 ft).

  6. en.wikipedia.org › wiki › Atlas_LV-3BAtlas LV-3B - Wikipedia

    The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. Manufactured by Convair, it was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets.

  7. Jan 12, 2024 · Atlas was a liquid propellant rocket burning RP-1 kerosene fuel with liquid oxygen in three engines configured in an unusual "stage-and-a-half" or "parallel staging" design: two outboard booster engines were jettisoned along with supporting structures during ascent, while the center sustainer engine, propellant tanks and other structural element...

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