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  •  ABSTRACT

  • - DESCRIPTION

  • - CONTAINER

  • - FLIGHT WITHOUT CONTAINER

  • - HEAD

  • - TAIL

  • - LOADING PHASES

  • - COMMAND CABLE

  • - CENTER OF GRAVITY

  • - RAILS AND LOCKING RACK

  • - VIRTUAL SIMULATION

  • - THREE-VIEW DRAWING

  • - RIGID STRUCTURE

  • - UNLOADING ANIMATION

  • - 2D IMAGES

  • - TECHNICAL PRECEDENTS

  • - IMAGES GALLERY

  • - FREQUENTLY ASKED QUESTIONS

  • - CONCLUSION

  •  

     

    They have been carried out tests of virtual simulation of the aircraft with software designed specifically for this function. A model was designed with the following data:
     
    Span: 26.6 m.
    Total longitude: 23.3 m.
    Total height: 7.5 m.
    Area of the wing: 700 pies˛.
    Area horizontal stabilizer: 178 pies˛.
    Area vertical stabilizer: 90 x 2 pies˛.
    Longitude of the container: 12 m.
    Longitude of the head: 4.7 m.
    Weigh maximum to take off: 18.000 kg. (with container and fuel)
    Weigh minimum: 8.000 kg. (without container neither fuel)
     
    Propellers:
    Power max. per engine 8000 feet/pound
    Diam. propeller: 13.5 feet
    No. blades: 4
     
    With the virtual tests, they were obtained been fully satisfactory flight test in the different suppositions to carry out for the aircraft.

    Antonio Sánchez 1997-2007. Málaga. Spain