Reference photo · Configuration may differ
Credit
U.S. Air Force photo by Master Sgt. Donald R. Allen · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
F-35C column in table headed F-35A / F-35B / F-35C; May 2020 manufacturer specification
Single sourceF-35C · Length
Single sourceConfiguration
| Specification | F-35C | Sukhoi Su-33 |
|---|---|---|
| Combat radius on internal fuel | 670 nmi (1,241 km)[source]F-35C; explicitly labelled CV CATOBAR column; Combat radius on internal fuel | — |
| Thrust/weight • full fuel: • 50% fuel: | 0.75 0.91[source]F-35C; explicitly labelled CV CATOBAR column; Thrust/weight • full fuel: • 50% fuel: | — |
| g limit | + 7.5[source]F-35C; explicitly labelled CV CATOBAR column; g limit | — |
| Role | carrier-based variant[source]F-35C; own variant section |
51.5 ft (15.7 m)[source]F-35C; explicitly labelled CV CATOBAR column; Length
51.5 ft / 15.7 m[source]F-35C column; Length; manufacturer specification dated 4 May 2020
Length
Single source21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
F-35C column in table headed F-35A / F-35B / F-35C; May 2020 manufacturer specification
Single sourceF-35C · Wingspan
Single source43 ft (13.1 m)[source]F-35C; explicitly labelled CV CATOBAR column; Wingspan
43 ft / 13.1 m[source]F-35C column; Wingspan; manufacturer specification dated 4 May 2020
Wingspan
Single source14.7 m (48 ft 3 in)[source]
F-35C column in table headed F-35A / F-35B / F-35C; May 2020 manufacturer specification
Single sourceF-35C · Height
Single source14.7 ft (4.48 m)[source]F-35C; explicitly labelled CV CATOBAR column; Height
14.7 ft / 4.48 m[source]F-35C column; Height; manufacturer specification dated 4 May 2020
Height
Single source5.93 m (19 ft 5 in)[source]
Empty; F-35C column; Weight empty; manufacturer specification dated 4 May 2020 · Empty weight
Single sourceEmpty; F-35C · Empty weight
Single source34,581 lb (15,686 kg)[source]F-35C; explicitly labelled CV CATOBAR column; Empty weight
70,000 lb (31,800 kg) class[source]F-35C; explicitly labelled CV CATOBAR column; Max takeoff weight
34,800 lb[source]F-35C column; Weight empty; manufacturer specification dated 4 May 2020
70,000 lb class[source]F-35C column; Maximum weight; manufacturer specification dated 4 May 2020
Empty; Empty weight
Single sourceGross; Gross weight
Single sourceF-35C · Combat radius on internal fuel
Single source>600 nm / 1,100 km (USN profile)[source]F-35C column; Combat radius (internal fuel); manufacturer specification dated 4 May 2020
2 × Saturn AL-31F3 afterburning turbofan engines thrust each dry
Single sourcewith afterburner
Single source2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 125.5 kN (28,200 lbf) with afterburner[source]
F-35C · Internal fuel
Single source19,750 lb (8,958 kg)[source]F-35C; explicitly labelled CV CATOBAR column; Internal fuel
F-35C column; Weapons payload; manufacturer specification dated 4 May 2020 · Payload
Manufacturer claimF-35C · Weapons payload
Single source18,000 lb (8,160 kg)[source]F-35C; explicitly labelled CV CATOBAR column; Weapons payload
18,000 lb / 8,160 kg[source]F-35C column; Weapons payload; manufacturer specification dated 4 May 2020
Service ceiling
Single source17,000 m (56,000 ft)[source]
48,400 ft/min
Single source246 m/s (48,400 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Introduction date | F-35C: 28 February 2019 (USN)[source]F-35C; explicitly named introduction date clause | 31 August 1998 (official)[source] |
|---|
| Horizontal tail span | 26.3 ft / 8.02 m[source]F-35C column; Horizontal tail span; manufacturer specification dated 4 May 2020 | — |
|---|
| Fuel capacity | 19,750 lb / 8,960kg[source]F-35C column; Internal fuel capacity; manufacturer specification dated 4 May 2020 | 9,500 kg (20,900 lb) internal[source] |
|---|
| Powerplant | F135-PW-100 40,000 lb Max. 25,000 lb Mil. Vertical N/A[source]F-35C column; Propulsion* (uninstalled thrust ratings); manufacturer specification dated 4 May 2020 | — |
|---|
| Maximum g-rating | 7.5[source]F-35C column; Max g-rating; manufacturer specification dated 4 May 2020 | — |
|---|
| Type | — | Carrier-based air superiority fighter with multirole capabilities[source] |
|---|
| National origin | — | Soviet Union Russia[source] |
|---|
| Manufacturer | — | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary user | — | Russian Navy[source] |
|---|
| Number built | — | 24 built total[source] |
|---|
| Manufactured | — | 1987–1999[source] |
|---|
| First flight | — | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Developed from | — | Sukhoi Su-27[source] |
|---|
| Variant | — | Shenyang J-15[source] |
|---|
| Guns | — | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | — | 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P Bombs: RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| g limits | — | + 8[source] |
|---|
| Wing loading | — | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Thrust/weight | — | 0.83[source] |
|---|
| Landing speed | — | 240 km/h (150 mph; 130 kn)[source] |
|---|
| Rockets | — | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Missiles | — | Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P[source] |
|---|
| Bombs | — | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; Max takeoff weight