Prospective Air Complex for Long Range Aviation (PAK DA) Specifications
guesstimates verging on speculation
Variant | |
Role | strategic bomber |
Country | Russia |
Builder | Tupolev |
First Flight | 202? |
Status | Development |
Number built | |
Operators | Russian Air Force |
Cost | |
Comparable Aircraft | B-21 |
Recognition | |
Wingspan | 20 meters | feet |
Wingspan | 20 meters | feet |
Sweep | |
Wing Aspect Ratio | |
Fuselage Maximum Diameter | meters | feet |
length | 42 meters | feet |
height | 8 meters | feet |
wing area | ~100 sqm | ~1100 sqfeet |
Weight empty | 45.000 kg | 100,000 lb |
takeoff (clean) | 90.000 kg | 200,000 lb |
takeoff (maximum) | 145-170,000 kg | 320,000-375,000 lb |
Fuel, Internal | not defined | lb |
Fuel, External | kg | lb |
Payload | 30 to 45 tons | 66,000-100,000 lb |
Max weapon load | kg | lb |
Armament |
4 x X-45 air-to-surface missiles
24 x X-2000
anti-ship missiles
high-precision bombs
defensive aircraft weapons
hypersonic weapons
VNIITF special air bombs
|
Power Plant |
4 x NK-32-2 (Product RF) or
4 x RD-36-41 (NK-101) |
Thrust, max, SLS, ISA | 4 x 16-24,000 kg | x lbst |
Internal fuel (usable) | kg | lb |
Performance (clean, ISA) | |
Max level speed (sea level) | subsonic |
Limit speed | 900 km/h |
Stall speed (landing, 20% fuel) | 90 KCAS |
Stall speed (reference) | KCAS |
Rate of climb (SL) | feet/min |
Service ceiling | 24,000 meters?? | 80,000 feet ?? |
Range / 3 ext. tanks (10% reserve) | N/A km | N/A nm |
Range, ext. tanks | N/A km | N/A nm |
Range, clean | 11,000-15,000 kilometers | nm |
Endurance, clean / ext. tanks | h min / hr |
Max sustained Load Factor (S.L.) | g |
Max sustained Load Factor (15,000 feet) | g |
Max sustained Turn Rate (15,000 feet) | deg/sec |
Takeoff ground run (S.L.) | 1.350/1.100 meters | feet |
Landing roll (S.L., 20% fuel?) | 950 meters | feet |
Limit Load factor | + g / - g |
Crew | 3-4 individuals |
Accomodations | |
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