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Weapons of Mass Destruction (WMD)


Prospective Air Complex for Long Range Aviation (PAK DA) Specifications

guesstimates verging on speculation
Variant
Rolestrategic bomber
CountryRussia
BuilderTupolev
First Flight202?
StatusDevelopment
Number built
OperatorsRussian Air Force
Cost
Comparable AircraftB-21
Recognition
Wingspan 20 meters feet
Wingspan 20 meters feet
Sweep
Wing Aspect Ratio
Fuselage Maximum Diametermeters 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
Payload30 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, ISA4 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 kmN/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
    Crew3-4 individuals
    Accomodations




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