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      1PipistrelAC

      Plpistrel-Sinus UL
      ProductID: AC-C-09
      Category: 複材機
      Unit: 架 >


     

    Plpistrel-Sinus UL


    前往 Pipistrel 專區,獲得更詳細的資訊及圖片!!


    200 公里巡航速度 暢遊藍天
    http://www.pipistrel.si/plane/sinus/overview
    超省油 --- 每小时仅 2.6 加仑 燃油消耗率
    200 公里 巡航速度
    1000 公里航程(標配油箱) (如用遠程油箱航程可達 1650 公里)

    Three aircraft in one
    Sinus combines a true sense of a motorglider with extreme efficiency during powered and long-range cruise flights. With the Sinus you can take off and land on very short runways, fly long distance cross-country and have fun gliding… all in



    Sinus UL 規格與性能

    model

    SINUS 912

    ENGINE ROTAX

    ROTAX 912 UL2

    max power(with 2 carb.)

    80 hp at 5800 rpm

    PROPELLER

    Pipistrel VARIO

    SIZES

     

    wing span

    14,97 m

    length

    6,6 m

    height

    1,70 m

    wing area

    12,26 m2

    rudder area

    1,1 m2

    tail area

    1,63 m2

    aspect ratio

    18,3

    positive flaps

    9 deg, 18 deg

    negative flaps

    5 deg

    center of gravity

    20% - 39%

    WEIGHTS

     

    empty weight

    285 kg

    empty weight light version

    275 kg

    max take off weight (MTOW)

    450 kg  / 472.5 kg / 544kg

    fuel tanks capacity

    2 x 30 l / 2 x 50 l

    useful fuel

    2 x 27 l / 2 x 45 l

    PERFORMANCES

    DATA PUBLISHED FOR TOM of 472.5 kg

    stall with flaps

    63 km/h

    stall without flaps

    66 km/h

    cruising speed (75% power)

    200 km/h   

    max. horizontal speed  

    220 km/h

    VNE

    225 km/h

    max speed with airbrakes out

    160 km/h

    max speed with flaps down

    130 km/h

    manoeuvring speed

    141 km/h

    best climb speed

    120 km/h

    max climb rate ( 450 kg)

    6,5 m/sec 

    climb rate at 140 km/h

    6,3 m/sec  

    min.sink speed

    90 km/h

    min.sink (prop. 90 deg.)

    1,03 m/sec

    max. sink with airbrakes

    5,5 m/sec

    best glide ratio speed

    95 km/h

    best glide (prop. 90 deg.)

    1:27

    glide at 150 km/h (prop 90 deg)

    1:18

    take off run ( 450 kg)

    88 m

    take off over 15 m obstacle (450 kg)

    148 m

    service ceiling ( 450 kg)

    8800 m

    45° - 45° roll time

    4,2 sec

    fuel consum. at cruis. speed

    9,2 l/hour

    endurance (std tanks)

    5,8 hours

    range distance

    1200 km

    max load factor permitted ( x 1,8)

    +4 g  - 2 g

    max load factor tested

    + 7,2 g - 7,2 g