Yahoo Web Search

Search results

  1. 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] Atlas was a liquid propellant rocket burning RP-1 kerosene fuel with liquid oxygen ...

    • December 17, 1957; 65 years ago
    • 1957–2010s (decade)
  2. Aug 21, 2002 · Atlas V is a two-stage launch vehicle. The first stage is comprised of a Russian-built RD-180 engine which burns a combination of liquid oxygen and RP-1 (kerosene) fuel. The first stage can produce a liftoff thrust of 933,406 pounds. The first stage can be augmented by up to five Aerojet strap-on solid rocket boosters.

  3. People also ask

  4. en.wikipedia.org › wiki › Atlas_VAtlas V - Wikipedia

    Atlas V [a] is an expendable launch system and the fifth major version in the Atlas launch vehicle family. It was originally designed by Lockheed Martin, now being operated by United Launch Alliance (ULA), a joint venture between Lockheed Martin and Boeing. It is used for DoD, NASA, and Commercial payloads.

    Flight No.
    Date And Time (utc)
    Type
    Serial No.
    100
    17 May 202422:16
    N22
    AV-085
    99
    6 October 2023 18:06
    501
    AV-104
    98
    10 September 2023 12:47
    551
    AV-102
    97
    10 November 2022 09:49
    401
    AV-098
    • US$110–153 million in 2016
    • 97, 401: 41, 411: 6, 421: 9, 431: 3, 501: 7, 511: 1, 521: 2, 531: 5, 541: 9, 551: 12, N22: 2
    • 2 (3 with Star 48 upper stage)
    • 21 August 2002, Hot Bird 6
  5. Atlas Mercury. Atlas-D, the first operational ICBM variant of the Atlas, was used to launch Mercury spacecraft on orbital missions. Ten Atlas-D rockets flew in support of project Mercury, including two failures and four manned missions. Mercury-Atlas 6, launched on 20 February 1962, placed John Glenn into orbit.

    • what kind of propellant was used in the atlas rocket launch1
    • what kind of propellant was used in the atlas rocket launch2
    • what kind of propellant was used in the atlas rocket launch3
    • what kind of propellant was used in the atlas rocket launch4
    • what kind of propellant was used in the atlas rocket launch5
  6. Apr 25, 2024 · The Atlas-Centaur rocket combined an Atlas first stage, which burned kerosene fuel, with a Centaur second stage, fueled with liquid hydrogen; it was the first rocket to use liquid hydrogen as fuel. Further versions of the Atlas included the SLV-3, a standardized launch vehicle designed for both military and civilian use that operated in various ...

    • The Editors of Encyclopaedia Britannica
  7. Aug 3, 2016 · Atlas-D Antares-2 American orbital launch vehicle variant with Atlas D first stage, Antares-2 solid propellant second stage. Concept ICBM American orbital launch vehicle. The January 1951 design for the Atlas used seven main engines plus two vernier engines to hurl the 3600 kg nuclear warhead over a 9300 km range.

  8. The Atlas 2AS is equipped with four strap-on solid rocket motors and is capable to lifting payloads of 3,719 kg (8,200 lb) into a geostationary transfer orbit. ATLAS STAGE. Size: 3.05-m Dia x 24. ...

  1. People also search for