| Model |
F-100A |
F-100C |
F-100D |
F-100F |
| Length |
47.8' |
47.8' |
49.3' |
52.5' |
| Span |
38.8' |
38.8' |
38.8' |
38.8' |
| Height |
15.5' |
15.5' |
16.2' |
16.2' |
| Crew |
1 |
1 |
1 |
2 |
| Engine |
J57-P-7/-39 |
J57-P-7/-21/-39 |
J57-P-21/-21A |
J57-21A |
| AC Electrical Power Source |
Three Inverters |
Three Inverters |
One Engine-Driven AC Generator w/One Stand-By Inverter |
One Engine-Driven AC Generator w/One Stand-By Inverter |
| Empty Weight |
18,185 lb |
19,270 lb |
20,638 lb |
21,712 lb |
| Gross Weight |
25,400 lb |
28,800 lb |
30,425 lb |
30,750 lb |
| Armament |
|
- Four 20mm Guns
- Various Combinations of External Loads Including Bombs, Rockets,
- Missiles Mounted on Removable Pylons
|
- Four 20mm Guns
- Various Combinations of External Loads Including Bombs, Rockets,
- Missiles Mounted on Force Ejection Pylons
|
- Two 20mm Guns
- Various Combinations of External Loads Including Bombs, Rockets,
- Missiles Mounted on Force Ejection Pylons
|
| Starter |
Pneumatic |
Pneumatic |
Pneumatic or cartridge |
Pneumatic or cartridge |
| Drop Tanks |
Two 275-Gallon |
Two 275-Gallon or 200-Gallon (Two 335 Gallon on Some Airplanes) |
Two 275-Gallon, Two 450-Gallon or Two 335 Gallon and/or Combination of 200-Gallon |
Two 275-Gallon, Two 450-Gallon or Two 335 Gallon and/or Combination of 200-Gallon |
| Internal Fuel |
Fuselage only |
Fuselage & wing |
Fuselage & wing |
Fuselage & wing |
| Refueling Provisions |
Gravity Tank Filling |
Pressure Type (Single Point and Air Refueling) |
Pressure Type (Single Point and Air Refueling) |
Pressure Type (Single Point and Air Refueling) |
| Flaps |
No |
No |
Yes |
Yes |
| Oxygen System |
Gaseous, w/D-2 Regulator |
Liquid, w/D-2A Regulator |
Liquid, w/MD-1 Regulator |
Liquid, w/MD-1 Regulator |
| Autopilot |
No |
No |
Yes |
Yes |
| Source: TO-1F-100D-1 |