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  2. Atlas (rocket family) - Wikipedia

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

    The first successful test launch of an SM-65 Atlas missile was on 17 December 1957. [1] Approximately 350 Atlas missiles were built. [4] The Atlas boosters would collapse under their own weight if not kept pressurized with nitrogen gas in the tanks when devoid of propellants. The Atlas booster was unusual in its use of "balloon" tanks.

  3. Jeanneau Yachts 65 - Wikipedia

    en.wikipedia.org/wiki/Jeanneau_Yachts_65

    The Jeanneau Yachts 65, also called the Jeanneau 65, is a French blue water cruising sailboat, that was first built in 2022. The hull was designed by Philippe Briand , the interior by Andrew Winch and finishing by the Jeanneau Design Office .

  4. SM-65F Atlas - Wikipedia

    en.wikipedia.org/wiki/SM-65F_Atlas

    The SM-65F Atlas, or Atlas-F, was the final operational variant of the Atlas missile, only differing from the Atlas E in the launch facility and guidance package used. It first flew on 8 August 1961, [1] and was deployed as an operational ICBM between 1961 and 1966.

  5. Porterfield Collegiate - Wikipedia

    en.wikipedia.org/wiki/Porterfield_Collegiate

    Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2760 and Simpson, 2001, p.442. General characteristics Crew: 2 Length: 22 ft 8 in (6.91 m) Wingspan: 34 ft 9 in (10.59 m) Height: 6 ft 11 in (2.11 m) Wing area: 168.80 sq ft (15.68 m 2) Empty weight: 671 lb (304 kg) Gross weight: 1,160 lb (526 kg) Powerplant: 1 × Continental A65-8/9 flat ...

  6. SM-65E Atlas - Wikipedia

    en.wikipedia.org/wiki/SM-65E_Atlas

    The SM-65E Atlas, or Atlas-E, was an operational variant of the Atlas missile. It first flew on October 11, 1960, and was deployed as an operational ICBM from September 1961 until April 1966.

  7. SM-65B Atlas - Wikipedia

    en.wikipedia.org/wiki/SM-65B_Atlas

    The Convair SM-65B Atlas, or Atlas B, also designated X-12 [1] was a prototype of the Atlas missile. First flown on 19 July 1958, the Atlas B was the first version of the Atlas rocket to use the stage and a half design with an operational sustainer engine and jettisonable booster engine section.

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