- United States
- Aircraft
- TC-135S Cobra Ball
| Category |
Fixed Wing |
Type |
Trainer |
| Year Commissioned |
1970 |
Year Decommissioned |
0 |
| Agility |
0.5 |
Damage Points (DP) |
20 |
| Empty Weight |
75160 kg |
Max Weight |
133633 kg |
| Runway Information |
2001-2600m TOD/LAD |
Physical Size |
Very Large Aircraft (26.1-75m) |
| Cost |
0 |
Hypothetical |
No |
| Payload Weight |
0 kg |
Crew |
10 people |
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Boom Refueling
| Model |
Purpose |
Range |
Scan Interval |
Generation |
|
AN/APQ-122(V)
|
Radar, Ground Mapping |
0.10 - 150.00 nm |
2 sec |
Early 1970s |
| Model |
Detection Angle |
Omnidirectional |
| AN/APQ-122(V) |
SB1, SB2, SMF1, PB1, PB2, PMF2 |
否 |
Weapon Loadouts Click to Expand Beta
| Loadout Type |
Role |
Ready Time |
Combat Radius |
| (Ferry) |
Ferry |
30 min |
5750 nm |
|
|
| (Reserve [Available]) |
Reserve |
180 min |
0 nm |
|
|
| (Maintenance [Unavailable]) |
Unavailable |
0 min |
0 nm |
|
|
| TELINT |
Area Surveillance |
180 min |
2870 nm |
|
|
| Type |
Front |
Side |
Rear |
| Visual Detection Range |
11.03 nm |
20.87 nm |
11.03 nm |
| Visual Classification Range |
4.18 nm |
8.23 nm |
8.08 nm |
| Infrared Detection Range |
7.35 nm |
13.67 nm |
18.62 nm |
| Infrared Classification Range |
3.48 nm |
6.86 nm |
3.48 nm |
| Radar, A-D Band (30-2000 MHz) |
17.5 dBsm (56.23 m²) |
19.4 dBsm (87.10 m²) |
17.5 dBsm (56.23 m²) |
| Radar, E-M Band (2-100 GHz) |
17.5 dBsm (56.23 m²) |
19.4 dBsm (87.10 m²) |
17.5 dBsm (56.23 m²) |
| Type |
Model |
Range |
Channels |
| Radio |
UHF/VHF Radio [Unsecure] |
100 nm |
0 |
| Radio |
HF Radio [Unsecure] |
300 nm |
10 |
| Model |
Type |
Engine Count |
Military Thrust |
Afterburner Thrust |
Military Fuel Rate (SFC) |
Afterburner Fuel Rate (SFC) |
Hypothetical |
Comments |
| 4x TF33-PW-5 |
Turbojet |
4 |
8172 |
- |
0.535 |
- |
No |
- |
| Fuel Type |
Fuel Capacity |
| Aviation Fuel |
70335 |