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DCS Reference/Missile Ranges
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| Name | Models and ranges | Note | |||||||
|---|---|---|---|---|---|---|---|---|---|
| AIM-7 “Sparrow” | E | F | M | MH | MH variant offers improved loft logic that allows for more efficient use of the flight energy. | ||||
| 24nm | 37nm | ||||||||
| 45km | 70km | ||||||||
| AIM-9 “Sidewinder” | B | J | L | M | P | P5 | X | X variant offers over-the-shoulder launching that significantly reduces effective range. | |
| 2.5nm | 10–15nm | 20nm | |||||||
| 4.5km | 18–27km | 37km | |||||||
| AIM-54 “Phoenix” | A Mk47 | A Mk60 | C Mk47 | C | The Mk60 engine offers higher acceleration and speed, and thus lower time on target, but also lower manoeuvrability. | ||||
| 100nm+ | |||||||||
| 180km+ | |||||||||
| AIM-120 AMRAAM | B | C | C variant has clipped wings for internal carry on the F-22, resulting in slightly lowered manoeuvrability. | ||||||
| 40nm | 57nm | ||||||||
| 75km | 105km | ||||||||
| R-3 / R-13 | M | M1 | R | S | All variants are based on the same K-13 platform reverse-engineered from the GAR-8 (AIM-9B). | ||||
| 8nm | 4.5nm | 4nm | |||||||
| 15km | 8km | 7km | |||||||
| R-27 | ER | ET | R | T | Guidance logic allows for a maximum vertical separation of ±10km (32k ft) for the R/T variants and ±12km (39k ft) for the ER/ET. | ||||
| 35nm | 28nm | 23nm | 18nm | ||||||
| 65km | 52km | 42km | 33km | ||||||
| K-55 / RS-2US | 3.5nm | All variants are based on the same K-5 platform, only with different seeker heads. | |||||||
| 6km | |||||||||
| R-60 | base model | M | The M variant has an 20° wider seeker FoV and significantly lower minimum range. | ||||||
| 4.5nm | |||||||||
| 8km | |||||||||
| R-73 | 16nm | Offers over-the-shoulder launching that significantly reduces effective range. | |||||||
| 30km | |||||||||
| R-77 | 54nm | ||||||||
| 100km | |||||||||
| R.550 | 8nm | ||||||||
| 15km | |||||||||
| Super 530D | 20nm | ||||||||
| 37km | |||||||||