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  2. Pentair - Wikipedia

    en.wikipedia.org/wiki/Pentair

    Pentair plc (PNR) is an American water treatment company incorporated in Ireland with tax residency in UK, with its main U.S. office in Golden Valley, Minnesota. [6] Pentair was founded in the US, with 65% of company's revenue coming from the US and Canada as of 2017.

  3. Reduced pressure zone device - Wikipedia

    en.wikipedia.org/wiki/Reduced_pressure_zone_device

    There is a variety of manufacturers of these gauges, but most utilize either a three-valve or a five-valve design to test the RPZD in different ways. In the UK , [ 6 ] Illinois, New York , [ 7 ] Texas , [ 8 ] and Missouri ( RsMO 10c60-11 ), the RPZD valve must be tested at least every 12 months by an accredited tester.

  4. AN/SPG-62 - Wikipedia

    en.wikipedia.org/wiki/AN/SPG-62

    The AN/SPG-62 is a continuous wave fire-control radar developed by the United States, and it is currently deployed on warships equipped with the Aegis Combat System. [1] It provides terminal target illumination for the semi-active SM-2MR/ER and ESSM Block 1 surface-to-air missiles.

  5. RIM-66 Standard - Wikipedia

    en.wikipedia.org/wiki/RIM-66_Standard

    A member of the Standard Missile family of weapons, the SM-1 was developed as a replacement for the RIM-2 Terrier and RIM-24 Tartar that were deployed in the 1950s on a variety of USN ships. The RIM-67 Standard (SM-1ER/SM-2ER) is an extended range version of this missile with a solid rocket booster stage.

  6. Standard Missile - Wikipedia

    en.wikipedia.org/wiki/Standard_Missile

    RIM-66 Standard MR/SM-2 missiles on a Mark 26 launcher, prior to being fired from the Aegis guided missile cruiser USS TICONDEROGA (CG-47) during tests near the Atlantic Fleet Weapons Training Facility, Roosevelt Roads, Puerto Rico.

  7. RIM-161 Standard Missile 3 - Wikipedia

    en.wikipedia.org/wiki/RIM-161_Standard_Missile_3

    The SM-3 evolved from the proven SM-2 Block IV design. The SM-3 uses the same solid rocket booster and dual thrust rocket motor as the Block IV missile for the first and second stages and the same steering control section and midcourse missile guidance for maneuvering in the atmosphere.