Comparison of Northrop Grumman B-2 Spirit and Tupolev Tu-95 [S]ave
| Attribute |  Northrop Grumman B-2 Spirit × |  Tupolev Tu-95 × |
|---|---|---|
| General | ||
| Manufacturer | Northrop Grumman | Tupolev |
| Model | Northrop Grumman B-2 Spirit | Tupolev Tu-95 |
| Country | United States | Russia |
| Manufactured from (year) | 1997 | 1956 |
| Manufactured to (year) | 2000 | 1993 |
| Type | Military Aircraft | Military Propellor Planes |
| Icao | B2 | TU95 |
| Performance | ||
| Engine | 4x 4 × General Electric F118-GE-100 | 4x 4 × Kuznetsov NK-12MV turboprops |
| Power, hp (hp) | - | 15,000 |
| Power, lbf (lbf) | 17,300 | - |
| Avionics | Honeywell and GEC Avionics | - |
| Max cruise speed (km/h) | 1,019 | 815 |
| Travel range (km) | 11,112 | 15,001 |
| Fuel economy (km/l) | 0.117 | 0.323 |
| Service ceiling (m) | 15,240 | 13,716 |
| Rate of climb (m/sec) | 15.24 | 10.16 |
| Take off distance (m) | 2,039 | - |
| Landing distance (m) | 1,052 | - |
| Weights | ||
| Max take off weight (kg) | 152,635 | 188,000 |
| Max payload (kg) | 20,000 | 5,000 |
| Fuel tank capacity (l) | 94,351 | 110,155 |
| Dimensions | ||
| Seats | 2 | 7 |
| Exterior length (m) | 21 | 49.1 |
| Tail height (m) | 5.18 | 13.4 |
| Fuselage diameter (m) | - | 2.9 |
| Wing span (m) | 52.4 | 50.1 |
| Wing tips | No Winglets | No Winglets |
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