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  2. Center of gravity of an aircraft - Wikipedia

    en.wikipedia.org/wiki/Center_of_gravity_of_an...

    The nose baggage compartment of a Fokker F.XII in 1933, avoiding the problem of heavy weights towards the rear Ballast Ballast is removable or permanently installed weight in an aircraft used to bring the center of gravity into the allowable range. Center-of-Gravity Limits

  3. Ballast - Wikipedia

    en.wikipedia.org/wiki/Ballast

    Ballast is dense material used as a weight to provide stability to a vehicle or structure. Ballast, other than cargo , may be placed in a vehicle, often a ship or the gondola of a balloon or airship , to provide stability .

  4. Ballast tank - Wikipedia

    en.wikipedia.org/wiki/Ballast_tank

    In the event of sudden changes in weather, such as wind gusts or temperature fluctuations, ballast can be adjusted to help keep the craft steady and reduce the risk of accidents. In many modern airships, automated systems are used to monitor and manage the ballast, ensuring the aircraft maintains the optimal weight and balance throughout the ...

  5. Rolladen-Schneider LS6 - Wikipedia

    en.wikipedia.org/wiki/Rolladen-Schneider_LS6

    Data from Jane's All the World's Aircraft 1988-89 [1] General characteristics. ... Max takeoff weight: 525 kg (1,157 lb) Water ballast: 140 L (37 US gal; 31 imp gal)

  6. Manufacturer's empty weight - Wikipedia

    en.wikipedia.org/wiki/Manufacturer's_empty_weight

    In aviation, manufacturer's empty weight (MEW) (also known as manufacturer's weight empty (MWE)) is the weight of the aircraft "as built" and includes the weight of the structure, power plant, furnishings, installations, systems, and other equipment that are considered an integral part of an aircraft before additional operator items are added for operation.

  7. Schempp-Hirth Discus - Wikipedia

    en.wikipedia.org/wiki/Schempp-Hirth_Discus

    Data from Jane's All the World's Aircraft 1988-89 [2] General characteristics. ... Max takeoff weight: 525 kg (1,157 lb) Water ballast: 180 L (48 US gal; 40 imp gal)

  8. Laister LP-15 Nugget - Wikipedia

    en.wikipedia.org/wiki/Laister_LP-15_Nugget

    The long span flaps serve both as speed-range drag reducing camber changing devices and full deflection high-lift/high-drag landing flaps. The aircraft can carry up to 185 lb (84 kg) of water ballast in a center fuselage tank, located at the center of gravity. The landing gear is a retractible monowheel. [1] [2]

  9. Schleicher ASH 26 - Wikipedia

    en.wikipedia.org/wiki/Schleicher_ASH_26

    Data from Jane's all the world's aircraft, 1992–93, [3] Schleicher ASH 26 E / ASH 26 brochure [4]. General characteristics. Crew: 1 Capacity: 110 kg (240 lb) water ballast Length: 7.55 m (24 ft 9 in)