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  2. Boeing C-17 Globemaster III - Wikipedia

    en.wikipedia.org/wiki/Boeing_C-17_Globemaster_III

    C-17 testing was limited to this lower weight. Airflow issues prevented the C-17 from meeting airdrop requirements. A February 1997 GAO report revealed that a C-17 with a full payload could not land on 3,000 ft (914 m) wet runways; simulations suggested a distance of 5,000 ft (1,500 m) was required. [30]

  3. Northrop Grumman RQ-4 Global Hawk - Wikipedia

    en.wikipedia.org/wiki/Northrop_Grumman_RQ-4...

    The UPA can support 1,200 lb (540 kg) of sensors and will create a canoe-shaped sensor bay on the fuselage's underside. [60] [61] Northrop Grumman also expects to receive a contract to integrate the UTC Aerospace Systems MS-177 multispectral sensor used on the Northrop Grumman E-8C JSTARS onto the RQ-4.

  4. USS San Antonio - Wikipedia

    en.wikipedia.org/wiki/USS_San_Antonio

    On 17 December 1996, the U.S. Navy awarded a contract to an industrial alliance led by Northrop Grumman Ship Systems (formerly Litton Avondale), with General Dynamics Bath Iron Works, Raytheon Electronic Systems and Intergraph Corporation, to design and construct the first of an anticipated 12 ships under the Navy's LPD-17 program.

  5. Grumman G-73 Mallard - Wikipedia

    en.wikipedia.org/wiki/Grumman_G-73_Mallard

    G-73 Mallard at the Air Zoo. Building on the success of the Goose and Widgeon, Grumman Aircraft developed larger G-73 Mallard for commercial use.Retaining many of the features of the smaller aircraft, such as twin radial engines, high wings with underwing floats, retractable landing gear and a large straight tail, the company built 59 Mallards between 1946 and 1951.

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    The search engine that helps you find exactly what you're looking for. Find the most relevant information, video, images, and answers from all across the Web.

  7. Kratos BQM-177 - Wikipedia

    en.wikipedia.org/wiki/Kratos_BQM-177

    Data from • Kratos Defense data sheet General characteristics Crew: None Length: 17 ft 0 in (5.18 m) Wingspan: 7 ft 0 in (2.1 m) Empty weight: 620 lb (281 kg) Max takeoff weight: 1,500 lb (680 kg) Fuel capacity: 63 gal Powerplant: 1 × MicroTurbo Tri 60-5 + turbojet, 1,000 lbf (4.4 kN) thrust Performance Maximum speed: Mach 0.95 References ^ a b "Kratos High Performance Target Drone System ...

  8. Rapid Dragon (missile system) - Wikipedia

    en.wikipedia.org/wiki/Rapid_Dragon_(missile_system)

    Rapid Dragon is a palletized and disposable weapons module which is airdropped in order to deploy flying munitions, typically cruise missiles, from unmodified cargo planes.. Developed by the United States Air Force and Lockheed, the airdrop-rigged pallets, called "deployment boxes," provide a low cost method allowing unmodified cargo planes, such as C-130 or C-17 aircraft, to be temporarily ...

  9. Ellison-Mahon Gweduck - Wikipedia

    en.wikipedia.org/wiki/Ellison-Mahon_Gweduck

    Data from Jane's All the World's Aircraft 2010/12 General characteristics Crew: Two pilots Capacity: 4 passengers Length: 34 ft 5 in (10.49 m) Wingspan: 48 ft 0 in (14.63 m) floats down Height: 10 ft 6 in (3.20 m) propellers "Y" Wing area: 295.0 sq ft (27.41 m 2) Aspect ratio: 7.8 Airfoil: GA35U-A315 Empty weight: 4,200 lb (1,905 kg) prototype Max takeoff weight: 5,999 lb (2,721 kg) Fuel ...

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