S-100
| Specifications | ||
|---|---|---|
| T-4 (Project) | "101" | |
| Powerplant | 4x jet engines | 4x RD36-41 |
| Thrust lb (kg) each | 33,060(15,000) | 35,262(16,000) |
| Length ft(m) | - | 145.96(44.5) |
| Wingspan ft(m) | - | 72.16(22) |
| Height ft(m) | - | 36.72(11.195) |
| Wing area ft^2 (m^2) | - | 3,182.62(295.7) |
| Max takeoff weight lb(kg) | 264,480 (120,000) | 275,500 (125,000) |
| Takeoff gross weight lb(kg) | 220,400-242,440 (100,000-110,000) | 251,256 (114,000) |
| Empty Weight | 55,600 kg | 122,542 (55,600) |
| Fuel Weight lb (kg) | - | 125,628 (57,000) |
| Wing loading lb/ft^2 (kg/m^2) | - | 78.54 (385) |
| Thrust-to-weight ratio | 0.545-0.6 | 0.56 |
| Cruise speed mph (km/h) | 1,863(3,000) | 1,987(3,200) |
| Range @ cruise speed (km) | 4000 km | |
| w/o drop tanks | 3,726(6,000) | 4,347(7,000) |
| w/drop tanks | 4,347(7,000) | - |
| Service altitude mi (km) | 13.66-14.90(22-24) | 12.42-14.90(20-24) |
| Takeoff run ft(m) | 5,576(1,700) | 3,116-3,280(950-1,000) |
| Landing run ft (m) | 1500 m | 2,624-3,116(800-950) |
| Landing speed | - | - |
|
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