- United States
- Aircraft
- TR-1A Dragon Lady
| Category |
Fixed Wing |
Type |
Recon |
| Year Commissioned |
1984 |
Year Decommissioned |
0 |
| Agility |
1 |
Damage Points (DP) |
10 |
| Empty Weight |
7264 kg |
Max Weight |
18598 kg |
| Runway Information |
250-450m (STOL) TOD/LAD |
Physical Size |
Large Aircraft (18.1-26m) |
| Cost |
0 |
Hypothetical |
No |
| Payload Weight |
2270 kg |
Crew |
1 people |
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Boom Refueling
Fuselage Structure - High-Altitude Slow-Speed Recon
| Model |
Purpose |
Range |
Scan Interval |
Generation |
|
TR-1 [IRLS]
|
IRLS, Non-Imaging Infrared Line Scanner |
0.00 - 5.00 nm |
10 sec |
Infrared, Non-Imaging |
|
TR-1 [OTHC]
|
Visual, Reconnaissance Very Long-Range Frame Camera |
0.00 - 80.00 nm |
10 sec |
Visual, 2nd Generation TV Camera (1980s/1990s, AXX-1 TCS) |
| Model |
Detection Angle |
Omnidirectional |
| TR-1 [IRLS] |
SMF1, SMF2, SMA1, SMA2, PMF1, PMF2, PMA1, PMA2 |
否 |
| TR-1 [OTHC] |
SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 |
是 |
Weapon Loadouts Click to Expand Beta
| Loadout Type |
Role |
Ready Time |
Combat Radius |
| (Ferry) |
Ferry |
30 min |
3500 nm |
|
|
| (Reserve [Available]) |
Reserve |
180 min |
0 nm |
|
|
| (Maintenance [Unavailable]) |
Unavailable |
0 min |
0 nm |
|
|
| Recon [Internal SLAR/IR] |
Unarmed Recon |
180 min |
1750 nm |
|
|
| Type |
Front |
Side |
Rear |
| Visual Detection Range |
4.81 nm |
6.74 nm |
4.81 nm |
| Visual Classification Range |
2.45 nm |
3.75 nm |
4.41 nm |
| Infrared Detection Range |
4.81 nm |
8.44 nm |
15.79 nm |
| Infrared Classification Range |
2.45 nm |
3.75 nm |
2.45 nm |
| Radar, A-D Band (30-2000 MHz) |
12.4 dBsm (17.38 m²) |
14.5 dBsm (28.18 m²) |
12.4 dBsm (17.38 m²) |
| Radar, E-M Band (2-100 GHz) |
12.4 dBsm (17.38 m²) |
14.5 dBsm (28.18 m²) |
12.4 dBsm (17.38 m²) |
| Type |
Model |
Range |
Channels |
| Radio |
UHF/VHF Radio [Unsecure] |
100 nm |
0 |
| Radio |
HF Radio [Unsecure] |
300 nm |
10 |
| AFSATCOM |
AFSATCOM |
0 nm |
0 |
| Skynet SATCOM |
Skynet SATCOM |
0 nm |
0 |
| Model |
Type |
Engine Count |
Military Thrust |
Afterburner Thrust |
Military Fuel Rate (SFC) |
Afterburner Fuel Rate (SFC) |
Hypothetical |
Comments |
| 1x J75-P-13B |
Turbojet |
1 |
7718 |
- |
0.79 |
- |
No |
U-2 |
| Fuel Type |
Fuel Capacity |
| Aviation Fuel |
8935 |