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  2. Sonex Aircraft SubSonex - Wikipedia

    en.wikipedia.org/wiki/Sonex_Aircraft_SubSonex

    The JSX-1 is a single place, single engine jet aircraft similar in design to an Onex, with a Waiex style Y tail, fixed main landing gear and a retractable nosewheel. Introduced at AirVenture 2009, it is powered by a Czech-built PBS TJ100 turbojet engine mounted above the aft fuselage, with the exhaust exiting between the Y-tail.

  3. Blohm & Voss P 178 - Wikipedia

    en.wikipedia.org/wiki/Blohm_&_Voss_P_178

    Data from Masters (1982). except where noted. General characteristics Crew: 1 Wingspan: 12.0 m (39 ft 4 in) Powerplant: 1 × Junkers Jumo 004 B turbojet, 8.8 kN (2,000 lbf) thrust (900 kg static thrust) Powerplant: 2 × (unknown make) rockets Armament Guns: 2 × 15 mm MG 151 /15 machine guns Bombs: 1 × 500 kg or 1 x 1,000 kg See also List of German aircraft projects, 1939–45 References ...

  4. Sonex Aircraft Sonex - Wikipedia

    en.wikipedia.org/wiki/Sonex_Aircraft_Sonex

    Sonex The original model, incorporating a low-wing design, seats two, and a conventional tail. Available as plans or a kit. [4] [12]Sonex B Introduced in April 2016, this model is a modification of the original Sonex, with an enlarged cockpit for larger and taller pilots, a center "Y-stick", electric flaps and dual throttles as standard.

  5. FMA IA-63 Pampa - Wikipedia

    en.wikipedia.org/wiki/FMA_IA-63_Pampa

    On 3 July 2019, Guatemala signed a contract worth $28 million for two Pampa III jet trainers. This made the Guatemalan Air Force the first export customer for the Pampa III. [ 18 ] [ 19 ] But one day after the purchase was made, the local representative of Transparency International accused President Jimmy Morales of avoiding local legislation ...

  6. Microturbo TRI 60 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRI_60

    The TRI 60 engine was developed in the 1970s to meet the need for a small, inexpensive, reliable, and expendable jet engine for use in cruise missiles and other small unmanned air vehicles. This need was broken down into the key requirements for high production at low cost and a high thrust-to-weight ratio. [ 2 ]

  7. Aero L-39 Skyfox - Wikipedia

    en.wikipedia.org/wiki/Aero_L-39_Skyfox

    Data from L-39 Next Generation web page General characteristics Crew: 2 Length: 11.83 m (38 ft 10 in) Wingspan: 9.37 m (30 ft 9 in) Airfoil: NACA 64A012 Empty weight: 3,100 kg (6,834 lb) Max takeoff weight: 5,800 kg (12,787 lb) Rear view of a L-39 Skyfox and its Williams FJ44 engine Powerplant: 1 × Williams International FJ44-4M turbofan engine, 16.89 kN (3,800 lbf) thrust Performance Maximum ...

  8. Cessna Citation family - Wikipedia

    en.wikipedia.org/wiki/Cessna_Citation_family

    The Cessna Citation is a family of business jets manufactured by Cessna that entered service in 1972. [1] In the fifty years following the type's first flight in 1969, more than 7,500 Citations were delivered, forming the largest business jet fleet in the world. [2]

  9. General Electric Passport - Wikipedia

    en.wikipedia.org/wiki/General_Electric_Passport

    The GE Passport is a high bypass ratio turbofan. The engine is a twin-spool, axial-flow turbofan with a high bypass ratio of 5.6:1 and an overall pressure ratio of 45:1. The front fan is attached to the three-stage low-pressure compressor; the 23:1 pressure ratio 10-stage high-pressure compressor includes five blisk stages for weight reduction.