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  2. Atlas V - Wikipedia

    en.wikipedia.org/wiki/Atlas_V

    As the Atlas V core is designed around RP-1 fuel and cannot be retrofitted to use a methane-fueled engine, a new first stage is being developed. This booster will have the same first-stage tankage diameter as the Delta IV and will be powered by two 2,400 kN (540,000 lb f ) thrust BE-4 engines.

  3. Comparison of orbital launch systems - Wikipedia

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

    Falcon 9 Block 5, the most prolific active orbital launch system in the world.. This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit.

  4. List of Atlas launches - Wikipedia

    en.wikipedia.org/wiki/List_of_Atlas_launches

    This is a list of launches made by the Atlas rocket family, derived from the SM-65 Atlas ICBM. The currently operational variant, Atlas V, has flown 81 consecutive missions without failure between October 2007 and January 2022. Due to the size of the list, it has been split by decade: List of Atlas launches (1957–1959)

  5. Atlas (rocket family) - Wikipedia

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

    The resulting conceptual heavy-lift vehicle was called "Atlas Phase 2" or "PH2" in the 2009 Augustine Report. An Atlas V PH2-Heavy (three 5 m stages in parallel; six RD-180s) along with Shuttle-derived, Ares V and Ares V Lite, were considered as a possible heavy lifter concept for use in future space missions in the Augustine Report. [29]

  6. Atlas LV-3B - Wikipedia

    en.wikipedia.org/wiki/Atlas_LV-3B

    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. With the ...

  7. Atlas I - Wikipedia

    en.wikipedia.org/wiki/Atlas_I

    Atlas I was the last use of the classic Atlas design with three engines, a jettisonable booster section, and two vernier engines. While retaining most of those features, Atlas II replaced the verniers with a hydrazine roll control system. [2] An Atlas I (serial number AC-69) on Pad 36B prior to launch of the CRRES satellite in 1990.