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  2. Northrop Grumman XRQ-73 SHEPARD - Wikipedia

    en.wikipedia.org/wiki/Northrop_Grumman_XRQ-73...

    The Northrop Grumman XRQ-73 SHEPARD (Series Hybrid Electric Propulsion AiRcraft Demonstration) is an hybrid-electric Group 3 unmanned aerial vehicle (weighting about 1,250 lb (570 kg)) developed by Northrop Grumman.

  3. Gulfstream American GA-7 Cougar - Wikipedia

    en.wikipedia.org/wiki/Gulfstream_American_GA-7...

    Data from FAA Type Certificate, The Incomplete Guide to Airfoil Usage, Pilot's Operating Handbook and Pilot Friend General characteristics Crew: one Capacity: three passengers Length: 28 ft 8 in (8.74 m) Wingspan: 36 ft 10 in (11.23 m) Height: 10 ft 4 in (3.15 m) Wing area: 184 sq ft (17.1 m 2) Airfoil: NACA 63A415 Empty weight: 2,569 lb (1,165 kg) Gross weight: 3,800 lb (1,724 kg) Powerplant ...

  4. Grumman XF10F Jaguar - Wikipedia

    en.wikipedia.org/wiki/Grumman_XF10F_Jaguar

    The Grumman XF10F Jaguar was a prototype swing-wing fighter aircraft offered to the United States Navy in the early 1950s. Although it never entered service, its research paved the way toward the later General Dynamics F-111 and Grumman's own F-14 Tomcat .

  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.

  6. Gulfstream III - Wikipedia

    en.wikipedia.org/wiki/Gulfstream_III

    The fuselage is 2 ft (0.6 m) longer aft of the main door, the radome is extended and there is a new curved windshield. Maximum takeoff weight is increased to 68,200 lb (30,935 kg) or 69,700 lb (31,615 kg) and there are various changes to the autopilot, flight instruments, and engine instruments.

  7. Grumman XP-50 - Wikipedia

    en.wikipedia.org/wiki/Grumman_XP-50

    The Grumman XP-50 was a land-based development of the shipboard XF5F-1 Skyrocket fighter, entered into a United States Army Air Corps (USAAC) contest for a twin-engine heavy interceptor aircraft. The USAAC placed an order for a prototype on 25 November 1939, designating it XP-50 , but it lost the competition to the Lockheed XP-49 .

  8. Grumman XF5F Skyrocket - Wikipedia

    en.wikipedia.org/wiki/Grumman_XF5F_Skyrocket

    The Grumman XF5F Skyrocket was a prototype twin-engined shipboard fighter interceptor. ... 303.5 sq ft (28.2 m 2) Empty weight: 8,107 lb (3,600 kg) Gross weight: ...

  9. Conair Firecat - Wikipedia

    en.wikipedia.org/wiki/Conair_Firecat

    Grumman S-2 Tracker The Conair Firecat is a fire-fighting aircraft developed in Canada in the 1970s by modifying military surplus Grumman S-2 Trackers . The modifications were developed by the maintenance arm of the Conair Group , which became a separate company called Cascade Aerospace .