Semi-active radar homing
, or SARH
, is a common type of missile guidance
system, perhaps the most common type for longer range air-to-air
and surface-to-air missile
systems. The name refers to the fact that the missile itself is only a passive detector of a radar signal – provided by an external ("offboard") source – as it reflects off the target.
NATO brevity code for a semi-active radar homing missile launch is Fox One.
The basic concept of SARH is that since almost all detection and tracking systems consist of a radar
system, duplicating this hardware on the missile itself is a waste. In addition, the resolution
of a radar is strongly related to the physical size of the antenna, and in the small nose cone of a missile there isn't enough room to provide the sort of accuracy needed for guidance. Instead the larger radar dish on the ground or launch aircraft will provide the needed signal and tracking logic, and the missile simply has to listen to the signal reflected from the target and point itself in the right direction. Additionally, the missile will listen rearward to the launch platform's transmitted signal as a reference, enabling it to avoid some kinds of radar jamming distractions offered by the target.
Contrast this with beam riding systems, in which the radar is pointed at the target and the missile keeps itself centered in the beam by listening to the signal at the rear of the missile body. In the SARH system the missile listens for the reflected signal at the nose, and is still responsible for providing some sort of "lead" guidance. The advantages are twofold. One is that a radar signal is "fan shaped", growing larger, and therefore less accurate, with distance. This means that the beam riding system is not terribly accurate at long ranges, while SARH is largely independent of range and grows more accurate as it approaches the target—the "source" of the signal it listens for. Another difference is that a beam riding system must accurately track the target at high speeds, typically requiring one radar for tracking and another "tighter" beam for guidance. The SARH system needs only one radar set to a wider pattern.
Modern SARH systems use continuous-wave
(CW) radar for guidance. Even though most modern fighter radars are pulse Doppler sets, most have a CW function to guide radar missiles. A few Soviet
aircraft, such as some versions of the MiG-23
, used an auxiliary guidance pod or aerial to provide a CW signal. The Vympel R-33
AA missile for MiG-31
interceptor uses SARH as the main type of guidance (with supplement of inertial guidance on initial stage).
SARH missiles require the tracking radar to lock on to the target and then illuminate it for the entire duration of the missile's flight. This could leave the launch aircraft vulnerable to counter attack, as well as giving the target's electronic warning systems time to detect the attack and engage countermeasures. Because most SARH missiles require guidance during their entire flight, older radars are limited to one target per radar emitter at a time.
Electronic counter-countermeasure (ECCM)
Recent-generation SARH weapons have superior electronic counter-countermeasure (ECCM
) capability, but the system still has fundamental limitations. Some newer missiles, such as the SM-2
, incorporate terminal semi-active radar homing (TSARH). TSARH missiles use inertial guidance
for most of their flight, only activating their SARH system for the final attack. This can keep the target from realising it is under attack until shortly before the missile strikes. Since the missile only requires guidance during the terminal phase, each radar emitter can be used to engage more targets. Some of these weapons, like the SM-2, allow the firing platform to update the missile with mid-course updates
The combat record of SARH missiles was unimpressive during the Vietnam War
and US Navy
fighters armed with AIM-7 Sparrow
attained a success rate of barely 10%, which tended to amplify the effect of deleting the gun on most F-4 Phantoms
, which carried 4 Sparrows. Some of the failures were attributable to mechanical failure of 1960s era electronics which could be disturbed by pulling a cart over uneven pavement, or pilot error; the intrinsic accuracy of these weapons was low relative to Sidewinder
and guns. However, since Desert Storm
, most F-15 Eagle
combat victories have been scored with the Sparrow at BVR
ranges. Also notable is the combat victory of an Israeli Eagle on one fast, high-flying MiG-25 Foxbat