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  2. Cessna CitationJet/M2 - Wikipedia

    en.wikipedia.org/wiki/Cessna_CitationJet/M2

    The CJ series are powered by two Williams FJ44 engines; the design uses the Citation II's forward fuselage with a new carry-through section wing and a T-tail. The original CitationJet model has been updated into the CJ1/CJ1+/M2 variants; additionally, the CJ1 was stretched into the CJ2/CJ2+ which was built between 2000 and 2016.

  3. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    This page is an incomplete list of orbital rocket engine data and specifications. Current, upcoming, and in-development rocket engines ... [1] 26,689 [1] 8.62 [1] 118 ...

  4. X-Plane (simulator) - Wikipedia

    en.wikipedia.org/wiki/X-Plane_(simulator)

    X-Plane is a flight simulation software initially launched by Laminar Research in 1995. Commercial desktop versions are sold for macOS , Windows , and Linux . In addition, Laminar Research also distributes FAA -certified versions for professional use.

  5. NASA X-57 Maxwell - Wikipedia

    en.wikipedia.org/wiki/NASA_X-57_Maxwell

    The experiment precedes the X-57 Maxwell X-plane demonstrator proposed under NASA's Transformative Aeronautics Concepts program. A piloted X-plane should fly within a couple of years, after replacing a Tecnam P2006T wings and engines with an improved version of the LEAPTech wing and motors. Using an existing airframe will allow engineers to ...

  6. Cessna Skymaster - Wikipedia

    en.wikipedia.org/wiki/Cessna_Skymaster

    Data from Jane's All The World's Aircraft 1969–70 General characteristics Crew: 1 Capacity: 5 passengers Length: 29 ft 9 in (9.07 m) Wingspan: 38 ft 09 in (11.81 m) Height: 9 ft 4 in (2.84 m) Wing area: 201 sq ft (18.7 m 2) Aspect ratio: 7.18:1 Airfoil: NACA 2412 at root, NACA 2409 at tip Empty weight: 2,655 lb (1,204 kg) Max takeoff weight: 4,400 lb (1,996 kg) Fuel capacity: 92 US gal (77 ...

  7. CFM International CFM56 - Wikipedia

    en.wikipedia.org/wiki/CFM_International_CFM56

    Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.

  8. Beechcraft Denali - Wikipedia

    en.wikipedia.org/wiki/Beechcraft_Denali

    The Beechcraft Denali, [3] also known as the Model 220 [2] and previously the Cessna Denali and Textron "Single Engine Turboprop" (SETP), is an American single engine turboprop aircraft under development by Textron Aviation. Announced at EAA AirVenture Oshkosh 2015, the aircraft is a completely new design, not derived from any existing aircraft ...

  9. Cessna Citation Mustang - Wikipedia

    en.wikipedia.org/wiki/Cessna_Citation_Mustang

    Cessna Citation Mustang instrument panel A Mustang PW615F engine uncowled. Data from Cessna Aircraft Company [14] General characteristics. Crew: one or two pilots; Capacity: 4 to 5 passengers and 3130 lb (1420 kg) useful load; Length: 40 ft 7 in (12.37 m) Wingspan: 43 ft 2 in (13.16 m) Height: 13 ft 5 in (4.09 m) Empty weight: 5,600 lb (2,540 kg)