Mitsubishi solitaire




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  • Solitaire и Marquise выпускались "Mitsubishi Aircraft International" до марта года. К этому времени построили 57 Solitaire и Marquise. Все машины семейства MU-2 имели аналогичную конструкцию. Крыло состояло из двух лонжеронов и панелей обшивки из алюминиевых сплавов и имело относительно небольшую площадь для самолетов такого класса (16,55 м2).

    Производитель: Mitsubishi, модель: Solitaire, год выпуска: , Регистрационный номер: NKB, местонахождение: США.

    ФАКТ! Компания Mitsubishi Group создана в Японии, в далеком 1870-м году. И с тех пор она ни разу не меняла свой логотип. Три известных ромба символизируют три бриллианта, «трех китов», на которых держится вся концепция концерна: честность, ответственность и готовность к сотрудничеству.

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    Первые работы над проектированием воздушного судна этой модели начались японскими инженерами в году, причём, благодаря совместной работе дизайнеров и авиастроителей удалось создать не только качественный, но и весьма перспективный самолёт, нашедший большую поддержку у заказчиков. Номер товара на eBay:. This calculation is performed by the pilot in command prior to every flight to ensure an adequate margin of safety in the event a take-off has to be aborted. В зависимости от модификации ; Масса пустого самолёта: Balanced field length is the distance required to bring the aircraft up to take off speed and slow it to a full stop at an average air density and payload.

    Mitsubishi MU-2 Solitaire (MU-2B) - Untitled | Aviation Photo # | FARM-AND-SERF.RU

    The cabin measures 8. The baggage compartment can hold up to 6. The Mitsubishi MU 2 Solitaire has a maximum range not including headwinds, high altitude, hot temperatures, or higher capacity of 1, miles and a maximum speed of mph. Common names and abbreviations: Passenger and baggage amounts can greatly effect the performance of an aircraft since minimum runway lengths, range and speed are all effected by its weight.

    Typical passenger configuration is the typical number of passengers the jet is configured to accommodate 5 passengers, however each jet will have a custom configuration to accommodate an owners specific needs and will therefore vary. Internal baggage capacity is the amount of available baggage which can be stowed inside the aircraft where there will be pressurization and temperature control. External baggage capacity is the amount of baggage space accessed from outside the aircraft and may not have pressurization or temperature control.

    Total number of bags is the total number of bags, using an average 5 cubic feet per bags plus 2 cubic feet of space between bags unusable space that you could expect to fit in the aircraft. Cruise speeds vary greatly during the course of a flight, during climb, cruise and descent. In addition, there is a speed limit of knots below 10, feet which will impact average speed for shorter flights greater than longer flights.

    Maximum cruise is the speed the aircraft can fly at its optimal altitude where the air is thinner. Average cruise is calculated by taking an average trip length and takes into account the climb, speed limit, cruise and descent speeds.

    Long range cruise is the speed required to attain the maximum range. Range varies depending on the weight of the baggage and passengers as well as the required runway length, altitude and speed during flight.

    Maximum range is the furthest the jet can fly at long range cruise speed at optimal altitude. Seats full range is the maximum range the jet will fly at long range cruise speed at optimal altitude with the maximum payload.

    Service ceiling is the maximum altitude the jet can fly. The higher the altitude, the thinner the air which allows the jet to fly faster and more efficiently since the thinner air produces less friction. Higher altitude can also make the flight more pleasurable since the pilots have more altitude options to avoid turbulence and adverse weather. Balanced field length is the distance required to bring the aircraft up to take off speed and slow it to a full stop at an average air density and payload.

    Balanced field length is effected by many factors such as altitude, temperature, humidity and the condition of the runway which is effected by rain and snow. This calculation is performed by the pilot in command prior to every flight to ensure an adequate margin of safety in the event a take-off has to be aborted.

    Landing distance is the amount of runway required to land the aircraft at an average weight and air density and will vary greatly for each mission. Useful payload is the amount of weight available after the weight of the pilot, crew and usable fuel have been deducted.

    Mitsubishi MU-2 & Spartan 7W Executive



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