table needs some work!
I will be grateful if you could help me with the correct translation table
I do. Is there an error range to account for weight reductions from advances in materials, manufacturing, and design?
It’s possible. But not for China in 2013
…
I, too, have something to thank you. You’re the first of the foreign users have given a link to my site. Thank you : Влюбленный:
http://www.flugzeugforum.de/suchoi-baut-kampfjet-5-generation-pak-fa-t-50-a-4550-3.html#post326169
To admit; this is the new generation of aerodynamic-specialists, who only take a look of a plane and instantly know the weight, the role, the weapons and avionics fit and even more all its weakpoints.
They are even so clever that even more if You show them images that a certain type is “not larger than” or even “smaller than”, if You show them aerodynamic analysis written by the designer they can turn that all down these arguments since they are “ALL-KNOWING”…
Tutorial “Designing aircraft” in 1983. The calculation is made according to the method described here. Have a question?
[ATTACH=CONFIG]217939[/ATTACH] [ATTACH=CONFIG]217940[/ATTACH]
Hardly. The right landing gear compartment, is the auxiliary power unit
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Estimated weight J-20
pilot weight of 100 kg
gun ammunition 150 kg
missiles, the normal load 950 kg
weapons, maximum load 6500 kg
propulsion weight 5976 kg
fuselage weight 4857 kg
the weight of the wing (2 pieces) 1100 kg
weight tails (2 pieces) 233 kg
chassis weight 603 kg
structural weight 6943 kg
weight 1894 kg of equipment
empty weight 17225 kg
curb weight airplane 17375 kg
normal takeoff weight of 26142 kg (50% of the fuel missiles)
maximum take-off weight of 32,908 kg (100% of the fuel missiles)
landing weight 18,246 kg
the maximum speed of 1,984 km / h (M = 1.87)
flight range of 3780 km
combat radius of 1,524 km
landing speed of 250 km / h
F-22 🙂
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J-31 – well
[ATTACH=CONFIG]217894[/ATTACH]
J-31 – poorly
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J-20 – poorly
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This pylon for missiles R-60 to the MiG-31
АПУ-60-II (П-62-2) – для УР Р-60 2-позиционное (2 missiles)
АПУ-60-IIМ (П-62-2М) – для УР Р-60 2-позиционное (2 missiles)
АПУ-60-IIМД (П-62-2МД) – для УР Р-60 2-позиционное (2 missiles)
АПУ-60-III (П-62-3) – для УР Р-60 3-позиционное (3 missiles)
[ATTACH=CONFIG]217650[/ATTACH]
amended version of the June 16, 2013
http://forum.keypublishing.com/attachment.php?attachmentid=217646&d=1371345390
I wonder if Paralay, when you have time, can you do your magic ( drawings) with this one as well ?:) ( i know it’s more difficult as we have no idea of the top configuration)
Let’s wait for the photos 🙂
The plant in Xian. Here can build a new plane.
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volume of 130 m3
washed area 651 m2
lift-drag ratio 14
the amount of weapons bays 19.3 m3 / 15%
fuel weight 35,300 kg
maximum thrust 9500 kg
afterburning thrust 15400 kg
propulsion weight 5976 kg
normal load of 6,000 kg
maximum load of 12,000 kg
fuselage weight 9122 kg
Wing weight 3030 kg * 2 = 6060 kg
weight of the fins 600 kg * 2 = 1200 kg
Chassis Weight 916 kg
empty weight of 26,190 kg
Curb weight 26340 kg
limit takeoff weight 74,000 kg (weapon 100%, 100% fuel)
maximum take-off weight of 67,800 kg
maximum range, the weight of 62000 kg
landing weight 28,300 kg
Thrust 0.417 – 0.65 kg / kg
Wing loading 326 – 511 kg / m
the maximum speed of 1,500 km / h
flight range of 7,000 km (range requires verification, probably more)
range of 2,400 km
landing speed of 213 km / h
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amended version of the June 16, 2013