Specifications (Tu-95MS)
General characteristics
* Crew: Seven - two pilots, one tailgunner, four others
* Length: 49.50 m (162 ft 5 in)
* Wingspan: 51.10 m (167 ft 8 in)
* Height: 12.12 m (39 ft 9 in)
* Wing area: 310 m² (3,330 ft²)
* Empty weight: 90,000 kg (198,000 lb)
* Loaded weight: kg (lb)
* Max takeoff weight: 188,000 kg (414,500 lb)
* Powerplant: 4× Kuznetsov NK-12MV turboprops, 11,000 kW (14,800 shp)[5] each
Performance
* Maximum speed: 925 km/h (500 kt, 575 mph)
* Range: 15,000 km (8,100 nm, 9,400 mi)
* Service ceiling: 12,000 m (39,000 ft)
* Rate of climb: 10 m/s (2,000 ft/min)
* Wing loading: 606 kg/m² (124 lb/ft²)
* Power/mass: 235 W/kg (0.143 hp/lb)
Armament
* Guns: 1 or 2× AM-23 23 mm cannon in tail turret
* Missiles: Up to 15,000 kg (33,000 lb), including the Kh-20, Kh-22, Kh-26, and Kh-55 air-to-surface missiles
* Bombs: 1 Atomic Bomb during Big Ivan test.
References
1. ^
http://www.fas.org/nuke/guide/russia/bomber/tu-95.htm
2. ^ FAS.org - "Tu-95 BEAR (TUPOLEV)"
3. ^ Aviation.ru - "Tu-20/95/142 Bear: The fastest prop-driven aircraft."
4. ^
http://www.dailymail.co.uk/pages/live/a ... ge_id=1770
5. ^ Originally measured as 15,000 PS.
Versus
Specifications (B-52H)
Orthographically projected diagram of the Boeing B-52 Stratofortress.
Data from Quest for Performance[1][16]
Maiden flight 1952-04-15
Introduction February 1955
General characteristics
* Crew: 5 — pilot, co-pilot, radar navigator (bombardier), navigator, and Electronic Warfare Officer; gunners are no longer a part of the crew.
* Length: 159 ft 4 in (48.5 m)
* Wingspan: 185 ft 0 in (56.4 m)
* Height: 40 ft 8 in (12.4 m)
* Wing area: 4,000 ft² (370 m²)
* Airfoil: NACA 63A219.3 mod root, NACA 65A209.5 tip
* Empty weight: 185,000 lb (83,250 kg)
* Loaded weight: 265,000 lb (120,000 kg)
* Max takeoff weight: 488,000 lb (220,000 kg)
* Fuel capacity: 47,975 US gal (181,725 L)
* Powerplant: 8× Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) each
* Zero-lift drag coefficient: 0.0119 (estimated)
* Drag area: 47.60 ft² (4.42 m²)
* Aspect ratio: 8.56
Performance
* Maximum speed: 560 knots (650 mph, 1,000 km/h)
* Combat radius: 4,480 mi (3,890 nm, 7,210 km)
* Ferry range: 11,000 mi (8,099 nm, 15,000 km)
* Service ceiling: 55,773 ft (17,000 m)
* Rate of climb: 6,270 ft/min[17] (31.85 m/s)
* Wing loading: 30 lb/ft² (150 kg/m²)
* Thrust/weight: 0.51
* Lift-to-drag ratio: 21.5 (estimated)
Armament
* Guns: 1× 20 mm M61 Vulcan cannon in a remote-controlled tail turret, now removed from all operational aircraft.
* Ordnance: up to 60,000 lb (27,200 kg) bombs, missiles, and mines, in various configurations