- France
- Aircraft
- F-8E Crusader
| Category |
Fixed Wing, Carrier Capable |
Type |
Fighter |
| Year Commissioned |
1963 |
Year Decommissioned |
1966 |
| Agility |
3.5 |
Damage Points (DP) |
5 |
| Empty Weight |
7956 kg |
Max Weight |
13000 kg |
| Runway Information |
901-1400m TOD/LAD |
Physical Size |
Medium Aircraft (12.1-18m) |
| Cost |
0 |
Hypothetical |
Yes |
| Payload Weight |
2300 kg |
Crew |
1 people |
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Probe Refueling
| Model |
Purpose |
Range |
Scan Interval |
Generation |
| AN/APQ-104 |
Radar, FCR, Air-to-Air & Air-to-Surface, Medium-Range |
0.10 - 60.00 nm |
2 sec |
Late 1970s |
| Model |
Detection Angle |
Omnidirectional |
| AN/APQ-104 |
SB1, PB2 |
否 |
Weapon Loadouts Click to Expand Beta
| Loadout Type |
Role |
Ready Time |
Combat Radius |
| (Ferry) |
Ferry |
30 min |
1230 nm |
|
|
| (Reserve [Available]) |
Reserve |
180 min |
0 nm |
|
|
| (Maintenance [Unavailable]) |
Unavailable |
0 min |
0 nm |
|
|
| A/A: R.550 Magic |
Air Superiority, WVR AAMs |
180 min |
150 nm |
|
|
| A/A: R.530 (SARH) |
Air Superiority, BVR AAMs |
180 min |
150 nm |
|
|
| Type |
Front |
Side |
Rear |
| Visual Detection Range |
2.77 nm |
6.03 nm |
2.77 nm |
| Visual Classification Range |
1.55 nm |
3.42 nm |
2.54 nm |
| Infrared Detection Range |
2.77 nm |
7.83 nm |
12.74 nm |
| Infrared Classification Range |
1.55 nm |
3.42 nm |
1.55 nm |
| Radar, A-D Band (30-2000 MHz) |
5.8 dBsm (3.80 m²) |
8.1 dBsm (6.46 m²) |
5.8 dBsm (3.80 m²) |
| Radar, E-M Band (2-100 GHz) |
5.8 dBsm (3.80 m²) |
8.1 dBsm (6.46 m²) |
5.8 dBsm (3.80 m²) |
| Model |
Comments |
| 20mm Mk12 x 4 [125 rnds x 4] |
Aircraft, F-8 |
| Type |
Model |
Range |
Channels |
| Radio |
UHF/VHF Radio [Unsecure] |
100 nm |
0 |
| Model |
Type |
Engine Count |
Military Thrust |
Afterburner Thrust |
Military Fuel Rate (SFC) |
Afterburner Fuel Rate (SFC) |
Hypothetical |
Comments |
| 1x J57-P-20A |
Turbojet |
1 |
4857 |
8490 |
0.81 |
2.22 |
No |
- |
| Fuel Type |
Fuel Capacity |
| Aviation Fuel |
4015 |