Page 81 - Combat Aircraft (January 2020)
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In the second half of a two-part feature, Combat Aircraft looks

                                                         at the most ambitious ‘Fulcrum’ derivative — the MiG-29M.
                                                         It was also used as a baseline for the MiG-29K shipborne
                                                         derivative, eventually ordered by India and Russia. After the
                                                         MiG-29K’s land-based export version was sold to Egypt, the
                                                         further improved MiG-35 was ordered for the Russian air arm.


                                                         REPORT AND PHOTOS Alexander Mladenov


                                                          The new intake FOD protection   this much heavier ‘Fulcrum’ derivative.
            MiG-29K AND MiG-35                           included a simpli  ed retractable system   The afterburning turbofan introduced
            SPECIFICATIONS                               of meshed grills preventing ingestion of   a new low-pressure compressor for a
                                                                                        greater mass-  ow. This, combined with
                                                         debris on take-o   and landing.
                                     MiG-29K   MiG-35     The revised wing design retained the   the higher-temperature turbine, resulted
             Dimensions                                  same span but was made capable of   in a signi  cant thrust increase compared
             Length                  17.30m  17.32m      carrying much greater weights, with a   with the baseline model. The new engine
             Wingspan                11.99m  11.99m      total of eight hardpoints — four under   had a hybrid digital/hydro-mechanical
             Height                  4.40m   4.40m       each console. The strengthened wing   control system for even better response.
             Wing area               42.00m 2  42.00m 2  structure enabled the MiG-29 to carry up   Rated at 86kN (19,400lb st or 8,766kgf)
             Weights                                     to 9,920lb (4,500kg) of ordnance.   at full afterburner, the RD-33K’s dry
             Normal take-o           18,550kg  17,500kg
             Maximum take-o          24,500kg  23,500kg   The undercarriage members were   rating was set at 53.96kN (12,122lb st or
             Maximum payload         6,500kg  6,500kg    reinforced — while remaining externally   5,500kgf).
             Performance                                 unchanged — in order to enable a   In its initial form, the MiG-29M boasted
             Maximum speed at sea level   1,400km/h  1,400km/h  maximum take-o   weight of more than   a much more modern cockpit layout,
             Maximum speed at high altitude   2,200km/h  2,100km/h  48,450lb (22,000kg).  with a pair of cathode ray tube (CRT)
             Ceiling                 17,500m  16,000m     More powerful Klimov RD-33K engines,   multi-function displays and hands on
             G limits                +9/-3   +9/-3       originally developed for the shipborne   throttle and stick (HOTAS) controls. It
             Range at high altitude on internal fuel  2,000km  2,000km  MiG-29K, were installed on the M version   had an all-new weapons control system
             Ferry range with three external tanks    3,000km  3,000km
                                                         in order to enhance the performance of   (WCS) centered on the then brand-

                                                                                                www.Key.Aero // January 2020  81




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        80-87 MiG-29 pt2 C.indd   81                                                                              21/11/2019   20:53
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