\u2028<\/p>\n Mikojan i Guriewicz MiG-29 is a front, one or two-seat fighter with twin-engined propulsion. The construction of a completely metal plane. The airframe together with the wide supporting hull and the hull parts of the wings form one integral unit that generates 40% of the lift of the aircraft. Vertical height doubled. The airframe withstands overloads +9 and -3g. The plane destroying value is over + 14g.<\/p>\n The MiG-29 has a band wing built from two parts: the basic one with a straight rake edge of 42 degrees and an auxiliary hull part with a curvilinear leading edge with a medium slant of 73 degrees. The wings are equipped with front flaps, rear flaps and ailerons.<\/p>\n The fuselage is based on two engine nacelles and a residual hull. Complete metal. In the front part there is a radiolocation station. The two-seater version does not have a radiolocation station. One or two-seater cockpit, equipped with catapult seats. The K-36 catapulted seat allows rescue in the speed range of 80 – 1,300 km \/ h from a height of 0 m. Fuel tanks are located in the central part of the airframe. The fuselage is finished with aerodynamic brakes.<\/p>\n The two motorized gondolas house the RD-33 engines. Air inlets adjustable and fitted with curtains that prevent foreign bodies from being sucked into the engine during take-off and roll-out. During this time, the air to the engine is sucked in by the upper blinds.<\/p>\n Vertical height doubled, divided into rudders and ballasts. Horizontal leveling of the plate type.<\/p>\n Three-point chassis with front support. The chassis is completely retracted to the airframe. The front of the shin has double wheels that are controlled. Main chassis with single wheels.<\/p>\n Mechanical control system with non-returnable hydraulic amplifiers. The control system has a system limiting the maximum values of the angle of attack.<\/p>\n The navigation system – MiG-29 received the inertial navigation system IK-WK-80-04 based on classical gyroscopes. The calculation of the aircraft’s location along with the necessary calculations for the automatic pilot is done by the central CWU-M navigation system operating in the 9-bit system. The data obtained by the inertial system are compared with the others, based on the count of the traveled distance (information of the aerodynamic data center SWS-P-72-3-2J). Definitely more accurate position correction is provided by a radio-based near-navigation system RSBN cooperating with terrestrial beacons of the RSBN system ("navigation" mode) or PRMG ("landing" mode). In emergency situations, the ARK-19 automatic radiocompass serves to assist the descent of the landing plane. In the MiG-29, the navigation equipment complements the RW-15 radio altimeter.<\/p>\n The MiG-29 defense system – The MiG-29 aircraft is equipped with a radiolocation radar warning station type SPO-15\u0141M and two 26 mm flare launchers and interfering dipoles placed on the extension of the vertical tail boards.<\/p>\n Radar R\u0141PK-29 Topaz N019.<\/p>\n In order to effectively use the carried weaponry, the aircraft was equipped with a SUW-29 weapon control system.<\/p>\n In Poland, MiG-29 aircraft have been modernized several times in order to be adapted to operate within the NATO armed forces.<\/p>\n The armor is suspended on 5 external weapon nodes. The weight of the weapon is 3 500 kg. As a standard, the central node is intended for an additional fuel tank. MiG-29 aircraft can carry projectile missiles, missile missiles and bombs. The main weapons are R-27, R-73 and R-60 missiles. During a typical air combat mission, the aircraft carried two R-27R missiles (on internal beams under wings) and four short-range R-60 or R-60M.<\/p>\n The complement to the missile weapon in the air combat is built permanently, on the left, 30 mm gun GSz-301 with a supply of 150 ammunition. The initial speed of the projectiles is 860 m \/ s with a rate of fire of 1500-1800 shots per minute.<\/p>\n As a drive, two turbine RD-33 turbines were used, created at OKB im. Klimowa from then Leningrad. The RD-33 was the first two-pass engine developed in CCCP for fighter aircraft. The engine tests on the dynamometer were carried out in 1972, and in 1981, its serial production was launched. A twin-engine drive system with widely spaced engines has a significant impact on the survivability of the aircraft if one of them hits. It takes about 1 hour to replace the engine. Lifespan of 350 hours.RD-33 is a two-shaft, two-flow motor with a 4-stage low pressure compressor (fan) and a 9-stage high pressure compressor. Behind the compressors are an annular combustion chamber and a 1-stage high and low pressure turbine. Behind the turbines and before the afterburner chamber, the exhaust gases mix with the cold external flow. The whole is completed with a supersonic, adjustable outlet nozzle.<\/p>\n The RD-33 engine without post-combustion has a maximum thrust of up to 2 x 49.92 kN, with unit fuel consumption reaching 0.079 kg \/ N \/ h. When using the minimum afterburning, the thrust reaches 2 x 54.91 kN, the maximum is 2 x 81.38 kN (then the fuel consumption reaches 0.210 kg \/ N \/ h). The engine length is 4 230 mm, the maximum diameter is 1000 mm and the weight of the dry engine is 1 055 kg. The engine version RD-33 D (R-33 D) has a string of 2 x 50.03 kN (2 x 5 100 kG), and with the afterburning 2 x 81.42 kN (2 x 8 300 kG).<\/p>\n MiG-29 has seven integral fuel tanks with a capacity of 4300 liters. Five of them were placed in the hull: 1-650 liters, No. 2-870 liters, No. 3-1810 liters and two marked as 3A placed symmetrically on the back of the hull with a capacity of 2 x 105 liters. Two additional tanks with a capacity of 2 x 330 liters were also placed in the wings. The tanks are filled through a central fuel fill or rain throat. It takes up to 20 minutes to refuel the aircraft together with the additional tank.<\/p>\n Written by Karol Placha Hetman<\/p>\n","protected":false},"excerpt":{"rendered":" Mikojan i Guriewicz MiG-29 is a front, one or two-seat fighter with twin-engined propulsion. The construction of a completely metal plane. The airframe together with the wide supporting hull and the hull parts of the wings form one integral unit that generates 40% of the lift of the aircraft. Vertical height doubled. The airframe withstands overloads +9 and -3g. The plane destroying value is over + 14g.<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"closed","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[41],"tags":[],"class_list":["post-1067","post","type-post","status-publish","format-standard","hentry","category-airplanes"],"_links":{"self":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/1067","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=1067"}],"version-history":[{"count":1,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/1067\/revisions"}],"predecessor-version":[{"id":4608,"href":"https:\/\/polot.net\/index.php?rest_route=\/wp\/v2\/posts\/1067\/revisions\/4608"}],"wp:attachment":[{"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=1067"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=1067"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/polot.net\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=1067"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}Construction MiG-29.<\/h3>\n
Wings.<\/h3>\n
Fuselage.<\/h3>\n
Tail-plane.<\/h3>\n
Wheeled chassis.<\/h3>\n
Systems in MiG-29.<\/h3>\n
Armament.<\/h3>\n
Drive.<\/h3>\n
Fuel tanks.<\/h3>\n
Data T-T MiG-29:<\/h3>\n