Do Tebe, který obvykle bazíruješ na naprostých detailech (osobně bych řekl blbostech  ), bych neřekl, že budeš plodit takovou koninu - to, že letadlo je druhému podobné, nic moc neznamená, obzvláště, když Tupolev je podstatně větší a hlavně s výrazně vyššími výkony...
Rockwell B-1b
Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
Length: 146 ft (44.5 m)
Wingspan:
Extended: 137 ft (41.8 m)
Swept: 79 ft (24.1 m)
Height: 34 ft (10.4 m)
Wing area: 1,950 ft² (181.2 m²
Airfoil: NA69-190-2
Empty weight: 192,000 lb (87,100 kg)
Loaded weight: 326,000 lb (148,000 kg)
Max takeoff weight: 477,000 lb (216,400 kg)
Powerplant: 4× General Electric F101-GE-102 augmented turbofans
Dry thrust: 14,600 lbf (64.9 kN) each
Thrust with afterburner: 30,780 lbf (136.92 kN) each
Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1-3 internal weapons bays each
Performance
Maximum speed:
At altitude: Mach 1.25 (830 mph, 1,330 km/h)
At low level: Mach 0.92 (700 mph, 1,130 km/h)
Range: 6,478 nmi (7,456 mi, 11,998 km)
Combat radius: 2,993 nmi (3,445 mi, 5,543 km)
Service ceiling: 60,000 ft (18,000 m)
Wing loading: 167 lb/ft² (816 kg/m²
Thrust/weight: 0.38
Tupolev Tu-160
Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
Length: 54.1 m (177 ft 6 in)
Wingspan:
Spread (20° sweep): 55.70 m (189 ft 9 in)
Swept (65° sweep): 35.60 m (116 ft 10 in)
Height: 13.10 m (43 ft 0 in)
Wing area:
Spread: 400 m² (4,310 ft²
Swept: 360 m² (3,875 ft²
Empty weight: 110 t[27] (242,000 lb)
Loaded weight: 267 tonnes[27] (590,000 lb)
Max takeoff weight: 275 tonnes[27] (606,000 lb)
Powerplant: 4× Kuznetsov NK-32[27] turbofans
Dry thrust: 137 kN (30,900 lbf) each
Thrust with afterburner: 245 kN (55,100 lbf) each
Performance
Maximum speed: Mach 2.05[28] (2,220 km/h, 1,380 mph) at high altitude
Range: 12,300 km[29] (7,643 mi) practical range without in-flght refuelling, Mach 0.77 and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves[29]
Combat radius: 7,300 km[27] (4,536 mi)
Service ceiling: 16,000 m[27] (49,200 ft)
Rate of climb: 70 m/s (13,860 ft/min)
Wing loading: 743 kg/m² with wings fully swept (152 lb/ft²
lift-to-drag: 18.5-19, while supersonic it is above 6.[30]
Thrust/weight: 0.37
Najdi deset rozdílů...
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Zdroj: wikipedia.org |
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