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 offer 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 |