R27er

In the same year, Vympel Design Bureau prepared technical proposals for a new K missile product designed to arm these promising aircraft, r27er. The development of the K was r27er to a team headed by A. Lyapin; the design was led by P, r27er.

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R27er

The high-explosive mass usually destroys any aircraft if hit directly. It is hard to dodge as well, since it is very fast, thus the target has very little time to react. It is incredibly fast especially at higher altitudes and maneuvers really well. Its practical range is almost comparable to the AIM Phoenix while being much harder to evade. Since the missile is a long-range BVR weapon, it is best used in a range of km. Before firing the missile off, the player should also climb to a higher altitude than the target and exceed Mach 1, as this will provide the missile more speed when being fired. Examine the history of the creation and combat usage of the weapon in more detail than in the introduction. Navigation menu Store Support Personal tools Log in. Namespaces Page Discussion. Views Read View source View history. Vehicles Aviation Ground vehicles Fleet. Navigation Recent changes Random page Help. From War Thunder Wiki. Jump to: navigation , search. This page is about the semi-active radar homing missile RER.

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It remains in service with the Russian Aerospace Forces , air forces of the Commonwealth of Independent States and air forces of many other countries as standard medium range air-to-air missile even though they have the more advanced R R family missiles are produced by both Russian and Ukrainian manufacturers. The R missile is also license-produced in China, [ citation needed ] though the production license was bought from Ukraine instead of Russia. RR and ER variants can be used in any meteorological conditions. RT and ET variants can be used out of cloudiness, at least 15 degrees away from the bearing of sun, and 4 degrees away from the bearing of moon and ground-based heat-contrasting conditions.

In the same year, Vympel Design Bureau prepared technical proposals for a new K missile product designed to arm these promising aircraft. The development of the K was entrusted to a team headed by A. Lyapin; the design was led by P. Dementiev and V. The prospect of simultaneous development of two fighters of almost identical purpose as early as at the stage of the technical proposal in prompted a fundamental decision to create a system of unified missiles: KA for the light MiG and KB for the heavy Su It was assumed that the missile versions would differ in terms of propulsion systems and, accordingly, launch range. On the basis of established practice, it was considered appropriate to provide for each version of the missile with different propulsion systems, with a "radius" and "thermal" CNS. This was the definition of the concept of a "modular" missile with variable COS and propulsion systems. It seemed very tempting to achieve interchangeability of propulsion systems by eliminating cable and gas connections of control equipment and gas generator in the central unit with the tail of the missile.

R27er

Soviet RR semi-active radar homing air to air missile on display in a museum. R long range air to air missiles on display in a museum. Note the pointed nose of the RR bottom and the round nose of the RT second from bottom. Source: Vitaly V. The R was designed to complement the R family of missiles. The R has a sleeker design and uses active radar homing guidance.

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In addition to the main version of the flight with the implementation of the proportional navigation method may apply special modes of guidance, providing more favorable modes of operation of the CNS and the radio detonator. The state tests were completed in The R was used by both sides during the Russian invasion of Ukraine. S2CID The final version was determined in , when the sketch design was issued, reflecting the requirements of the decrees of January 19, , which specified the requirements for MiG and Su respectively. The draft design of the active CLO was released back in View cart. The P missile is designed in a scheme that is intermediate between a "duck" scheme and a scheme with a swivel wing, with tandem-positioned stabilizers, rudders and wings see projections. The first thermal launches of La missiles were also made from the Su prototype, the T aircraft. The following year, 24 more missiles of various configurations were launched, including three combat missiles, completing the first stage of state trials on the MiG

In the late s, as part of the second generation upgrade program for the R family of missiles, a new motor with almost twice the speed and range replaced the older one, as per the modular design of the R family. The resulting heat-seeking variant, dubbed the RET, also received upgraded electronics, resulting in better tracking and slight weight savings. This missile would go on to fill the role of a fire-and-forget medium-long range missile for not only the Soviet air force, but its successor nations and all the export operators who flew the MiG and Su

The Drive. The fourth compartment is the combat unit of shrapnel-phase or rod type with the weight of 39 kg explosive charge weight - 15 kg. The high-explosive mass usually destroys any aircraft if hit directly. The creators of the missiles were awarded the State Prize in Track my order s. It was assumed that the missile versions would differ in terms of propulsion systems and, accordingly, launch range. The missile was not offered to the foreign market for a long time, but in it was demonstrated at the Fidae exhibition. Read Edit View history. According to the advertising information, the last RP1 variants have a range of 75 km when shooting at the rear hemisphere RHF and km when shooting at the front hemisphere RHF on a fighter target. ShVAK Recommended Kit. Navigation menu Store Support Personal tools Log in. It seemed very tempting to achieve interchangeability of propulsion systems by eliminating cable and gas connections of control equipment and gas generator in the central unit with the tail of the missile.