Su-17 Fitter vs Su-25 Frogfoot
Overview
The Su-17 Fitter and the Su-25 Frogfoot are both Combat Aircraft, manufactured by Sukhoi and Sukhoi respectively.
The Su-17 Fitter reaches 2,140 km/h — 2.2x the Su-25 Frogfoot's 970 km/h. The Su-17 Fitter has an operational range of 1,150 km vs 1,000 km for the Su-25 Frogfoot. The Su-17 Fitter operates at altitudes up to 14,500 m compared to 7,000 m for the Su-25 Frogfoot. At 17,600 kg MTOW, the Su-25 Frogfoot is 2.2x the Su-17 Fitter's 7,890 kg.
The Su-17 Fitter has been produced in 2,867 units vs 1,000 for the Su-25 Frogfoot. Unit cost is $6M for the Su-17 Fitter vs $11M for the Su-25 Frogfoot. The Su-17 Fitter first flew 9 years before the Su-25 Frogfoot (1966 vs 1975).
| Soviet-era fighter-bomber, extensively deployed in varied conflicts worldwide, known for its variable-sweep wing design and robust operational capacity. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Combat Aircraft |
| Manufacturer | Sukhoi |
| First flight | 1 January 1966 |
| Year introduced | 1971 |
| Number produced | 2867 units |
| Average unit price | $6 million |
| Soviet close air support aircraft, prominent during Afghan War, designed for ground targets engagement under heavy fire conditions. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Combat Aircraft |
| Manufacturer | Sukhoi |
| First flight | 22 February 1975 |
| Year introduced | 1981 |
| Number produced | 1000 units |
| Average unit price | $11 million |
| Wing area | 27.5 m² ◉ |
| Wingspan | 10.0 m â—‰ |
| Height | 4.5 m â—‰ |
| Length | 15.3 m â—‰ |
| Maximum speed | 2140 km/h â—‰ |
| Operational range | 1,150 km â—‰ |
| Service ceiling | 14,500 m â—‰ |
| Max. takeoff weight | 7,890 kg â—‰ |
| Empty weight | 5,932 kg â—‰ |
| Total thrust | 1 x 4,000 kgf â—‰ |
| Wing area | 30.1 m² ◉ |
| Wingspan | 14.4 m â—‰ |
| Height | 4.8 m â—‰ |
| Length | 15.5 m â—‰ |
| Maximum speed | 970 km/h â—‰ |
| Operational range | 1,000 km â—‰ |
| Service ceiling | 7,000 m â—‰ |
| Max. takeoff weight | 17,600 kg â—‰ |
| Empty weight | 9,500 kg â—‰ |
| Total thrust | 2 x 4,100 kgf â—‰ |
Performance Radar Chart
Detailed Comparison
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