| Engine |
|
|||||
|---|---|---|---|---|---|---|
| Engine name | Number | Basic mass | Wing loading |
|
|
|
| General Electric J85-GE-21A | kg | kg/m2 |
Payload weight:
|
|||
| Engine characteristics | Mass with fuel |
Max Gross Weight |
||||
| Weight (each) | Type | 30% (m) |
% (m)
|
% (m) | ||
| kg | Afterburning axial-flow turbojet | kg | kg | kg | kg | |
| Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | |||||
| Condition | 100% | WEP | ||||
| Stationary | kgf | kgf | ||||
| Optimal | kgf ( km/h) |
kgf ( km/h) |
||||
