DCS WORLD AIM 7 VS AIM 120 F18 FULL

The RIM-7H was a basic RIM-7E missile better adapted for shipboard use. AIM-7Gĭesigned for use with the F-111D 'Aardvark' but never taken into production. The missile was relatively short-lived because further development was cancelled in favor of a ship-launched derivative of the AIM-7M, the RIM-7M. The RIM-7F Sea Sparrow was the ship-launched equivalent of the AIM-7F.

Equipped with a dual-trust rocket motor for increased range and a completely new electronic guidance and control system compatible with pulse-doppler radars. Introduced in 1972, featuring a radical improvement over previous versions. The missile was essentially an unchanged AIM-7E and was fired from a modified ASROC launcher. This missile was known as RIM-7E Sea Sparrow. In 1967 a derivative of the missile was developped for use on ships to provide them with a missile based anti-aircraft defence system. The AIM-7E-3 had higher reliability and the AIM-7E-4 was specially adapted for use with high-power fighter radars (like the F-14's AN/AWG-9). This led to the development of the AIM-7E-2 which had a shorter minimum range and clipped wings for better manoeverability.

DCS WORLD AIM 7 VS AIM 120 F18 FULL

This increased performance could not be exploited to full extend due to limited IFF capabilities which required a visual identification of the target. It featured a new propulsion system based on a solid-fueled rocket which gave the missile an increased range and performance. (USAF photo)Introduced in 1963 and heavily used in Vietnam in conjunction with the venerable F-4 'Phantom'. The second YF-16 ( #01568), equiped with 2x AIM-9, 2x AIM-7 and camera pods test-firing a Sparrow missile. AIM-7DĪn AIM-7C with a new Thiokol LR44-RM-2 storable liquid-propellant rocket engine and an improved guidance system for better anti-jamming performances.

It featured a 65 lb (30 kg) MK 38 continuous-rod warhead and was propelled with a solid-fueled rocket engine. The missile was equipped with a semi-active homing radar. Intended for use with the Douglas F5D 'Skylancer' fighter and the Canadian CF-105 'Arrow' fighter but cancelled in 1958. This caused the missile to be withdrawn within a few years of service. The missile was equipped with a beam-riding guidence system which gave it a poor low-level performance and necessitated a visual identification of the target, making the missile not a BVR but VFR missile. Original design for use with the F3H-2M 'Demon' and F7U-3M 'Cutlass' fighters. The solid-propellant rocket motor provides the missile's propulsion. The missile is controlled by the flight control system via four movable delta wings and overall stability is provided by four fixed delta fins which are located in line with the forward wings. The missile is detonated with an active RF fuze when it comes within range of the projected target. The radar guidence system processes radar signals received from the launch aircraft's radar via its rear signal receiver, and also processes RF energy reflected from the target received by its own internal radar receiver.

Dcs world aim 7 vs aim 120 f18