I’ve heard that can be hung further 2 R-37M under the wing. MiG-31M could take six R-37 under the fuselage and two under the wing (8 R-37).
Gun MiG-31BM naturally remained in place.
source: Overscan
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The 1.1m diameter, 30cm deep, phased array antenna weighs 300kg, the whole radar weighing in at 1000kg.
Good to hear that you built Mig-31 with your own hands. Do you mind sharing some of your experiences with us. Compared to Su-27 was it really a complex aircraft to build.
Before stopping production, I did cowl guns MiG-31B and titanium engine compartment hatches on the MiG-31M. Complexity only in the materials used. Steel and titanium are difficult to process, duralumin – pleasant.
In the photo, assembly shop fuselages. Previously, there were built MiG-25 (pictured), now there are rusting MiG-31 🙂
I with my own hands built MiG-31 to 1994 plant “Sokol” stopped. In the shops of the plant remained 5 MiG-31B and 1 MiG-31M. Theoretically they can finish. Really – it is unlikely that it will do. MiG-31M – will not finish, that’s for sure.
T-50 will replace the MiG-31 after 2017. There is no point in starting a new program of modernization. Prior to 2018, if my memory serves me, modernize the remaining MiG-31B in the MiG-31BM. In the near future a number of aircraft to alter in a different version and the case closed.
good :rolleyes:
The engine has a specific density of the design. Engine compartment – will not change. That is the volume and weight of the motor can not change much.
I can calculate the center of gravity of the fighter, it will find the weight of the engine. I did it for the T-50 aircraft, but used outdated drawing. Motor weight – 1900 kg. Maybe I’ll correct account this weekend.
Some dubious figures, I think this is attributed to the journalists to create a sensation. I like this would be correct:
*
“izd. 99” (Su-27), 12,500 kg thrust, engine weight 1530 kg, the weight of 1530 kg / 12500 kg = 0.1224
“izd. 117S” (Su-35), thrust 14500 kg., engine weight 1520 kg, the weight of 1520 kg / 14500 kg = 0.105 (- 16.5%)
“izd. 117” (T-50), 15 500 kg of thrust, the engine weight ~ 1500 kg, the weight of 0.097 (- 26%)
“izd. 30” (T-50M), 17500 kg thrust, engine weight ~ 1500 kg, the weight of 0.086 (- 42%)
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