RuAF News and development Thread part 15

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Member for

15 years 3 months

Posts: 6,441

Does this seem correct?

The performance characteristics of the aircraft :
The crew - 1 person

Su-35 / T-10M / T-10BM / Su-35S

Length 22.18 m 21.95 m
Wingspan 14.7 m 14.75 m
Height 6.35 / 6.43 m 5.92 m
wing area 62.04 sq.m. 62.2 m
Sweep angle on the leading edge of the wing 42 degrees. 42 degrees.
Wing loading at normal weight
414 kg / m 410 kg / m
Wing loading at the maximum weight 548 kg / m 611 kg / m
Thrust-weight ratio with normal weight 0.97 1.14
Thrust-weight ratio with a maximum weight 0.74 0.76
Take-off weight maximum 34000 kg 34500 kg
Take-off weight is normal 25700 kg 25300 kg (2 x P-77, P-2 x 73)

empty weight 18400 kg 19000 kg
Fuel Weight with PTB 14300 kg
Weight without fuel PTB
10250 kg 11500 kg
Payload mass 8000 kg 8000 kg
The speed at maximum height 2,500 km / h / 2.35M 2,500 km / h / 2.35M
2.25 M (altitude 11,000 m)
2,400 km / h (in the first phase of the CIO in 2011)
Maximum speed at ground 1400 km / h / 1.17 M 1400 km / h / 1.17 m (height 200 m, confirmed during the first phase of the CIO in 2011)

Maximum speed without afterburner
over 1,300 km / h (over 1.1 M)
in the first prior art T-10BM - 1.1 M
cruising speed 800-950 km / h / 0.75-0.9 M
Range with max 1 refueling 6300 km
Flight range with maximum PTB 4500 km (at an altitude of 2 x FTB-2000)
Range maximum without PTB
3400 km 3600 km (altitude, speed cruising)
Distance from land flight (speed - 0.7 m)
1580 km
Combat radius of action 1,600 km
The ceiling is a practical 18000 m 18000/19000 m
18000 m (in the first phase of the CIO in 2011)
rate of climb more than 280 m / s more than 280 m / s
Acceleration time at a height of 1000 m at the fuel balance of 50% of the normal refueling 600 km / h up to 1100 km / h - 13.8 to
1100 km / h up to 1300 km / h - 8
Maximum operating overload 9G
Area EPR (estimated) 0.5-2 m
run 400-450 m (normal takeoff weight, full afterburner)

Mileage 650-700 m (with brake parachute and normal landing weight)

Member for

8 years 6 months

Posts: 906

Does this seem correct?

The performance characteristics of the aircraft :
The crew - 1 person

[CENTER]

Looks reasonable. and the empty weight.. well really reminds me of the Su-37.

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12 years 3 months

Posts: 307

Thanks TR1 for the pics. When I look at the factory I say to myself, no wonder they are not jumping straight to production of the Pak-Da. The work area looks so soviet era.
With the new Tu-160 being made first with new internal electronics etc and money being invested in new production machinery etc you would only then start Pak-Da production. The new Tu-160 gives the factory floor time to catch up in tooling, floor efficency, floor ergonomics etc.

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15 years 3 months

Posts: 6,441

Why not go for new multi function display in cockpit, when you build new airframe?

Member for

12 years 4 months

Posts: 2,171

Why not go for new multi function display in cockpit, when you build new airframe?

Wat. And where exactly do you see a new frame? You do realize they are modernizing Tu-160 to Tu-160M there and that we see the cockpit of the standard Tu-160?

We have no idea what Tu-160M2's cockpit will look like, and it is likely no-one does at this point.

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13 years 5 months

Posts: 9,579

Thanks TR1 for the pics. When I look at the factory I say to myself, no wonder they are not jumping straight to production of the Pak-Da. The work area looks so soviet era.
.

Well that make sense, that part of the plant has basically done nothing but modernize (slightly) a few air frames since Soviet times.

http://bmpd.livejournal.com/1789414.html

MiG-29s in Armenia.

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13 years 7 months

Posts: 31

First modernised Il-76MD. IL-76MDM - the project of modernization of aircraft Il-76M and Il-76MD designed to "Ilyushin" on the technical task of the Air Force issued in 2011 (ROC "Kuznetsk").

http://www.airliners.net/photo/2793787/L/

http://ic.pics.livejournal.com/foxbatru/14316787/246019/246019_original.jpg

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12 years 4 months

Posts: 2,171

After Syria this is hardly a surprise but Su-35S' that are doing combat patrol/QRA has now received R-77-1. Now, where is that R-37M...

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8 years 6 months

Posts: 906

After Syria this is hardly a surprise but Su-35S' that are doing combat patrol/QRA has now received R-77-1. Now, where is that R-37M...

Soon maybe :D

Member for

13 years 5 months

Posts: 9,579

After Syria this is hardly a surprise but Su-35S' that are doing combat patrol/QRA has now received R-77-1. Now, where is that R-37M...

Uh, was there supposed to be a video with this comment?

Hook a brother up.

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12 years 4 months

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No video. Just info from the infamous guy from Airforce.ru ;)

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8 years 6 months

Posts: 906

I found some nice cross sectional image of Russian AAM's like R-77 and R-33..like this one from testpilot.ru

http://www.testpilot.ru/russia/vympel/r/33/images/r33_s.jpg

you guys think that cross section image are good to scale ? I'm thinking of measuring dimensions of the rocket motor of the missile based on the image.

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9 years 10 months

Posts: 612

My point is, all the talk about su-33 is a better choice than the Su-30sm for a su-24 replacement in crimea, which started in thread #338, is pure fantasy

Ah, sorry, yes, of course. I missed that post as I don't take the author seriously.

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13 years 5 months

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Nice photo of VKS hardware in Syria:

https://c2.staticflickr.com/2/1709/25787772826_b8b7cdd7eb_o.jpg

330 sorties:

https://c2.staticflickr.com/2/1637/25720038531_b8a0193bde_o.jpg

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11 years 3 months

Posts: 150

. .
http://cdn-www.airliners.net/aviation-photos/middle/6/6/5/2794566.jpg

http://cdn-www.airliners.net/aviation-photos/middle/7/6/5/2794567.jpg

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20 years 4 months

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http://nortwolf-sam.livejournal.com/1203821.html

Apparently MOD is ordering land based Redut-Poliment complex.

IT would be logical to use the 9M96 with AESA on ships and convert it to land based system , Much like Aster or Israel MR-SAM program