Triode
Posts: 283
Joined: 9/26/2014 Status: offline
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[UPDATED DB pre-v437] quote:
ORIGINAL: Sunburn Thanks! Does the testing of PBK-500U in 2014/15 on Akhtubinsk mean the weapon has not yet entered RuAF service? Also, does the preference for the Kh-38 mean that the various Kh-25 upgrades (Kh-25MSE, Kh-25MAE etc.) were private-venture projects which were not adopted? Furthermore, what is happening with the various next-gen AAM projects? (RVV-MD, RVV-SD and RVV-BD) 1.Akhtubinsk not only test weapons, they created "Rules for use X from Y" for this weapons so in 2010 PBK-500U enter service with Su-34 , in 2014-2015 they test PBK-500U for Su-30SM and Su-35 2.Yes, an attempt from KTRV to sell "upgraded Kh-25" to some foreign users of Kh-25, zero success so far 3.in 2014-2015 Akhtubinsk test three AAM articles: 810,180,760 810 (RVV-BD) Guidance system - inertial with radio correction and active radar homing in on the final trajectory. launch range, the maximum in the PPP, for some types of targets, km - 200 the height of the target, km - 0,015-25 overload of the target, g - 8 starting weight, kg - not more than 510 angles targeting - ± 60 ° Warhead weight, kg - 60 length, m -4.06 Diameter, m - 0.38 wingspan, m - 0.72 the scope of the rudders, m - 1.02 180 (RVV-SD) Guidance system - inertial with radio correction and active radar homing in on the final trajectory. launch range: maximum km - 110 minimum, km - 0.3 the height of the target, km - 0,02-25 overload for the target, g - 12 starting weight, kg - not more than 190 Warhead weight, kg - 22.5 length, m - 3.71 Diameter, m - 0.2 wingspan, m - 0.42 the scope of the rudders, m - 0.68 760 (RVV-MD) Short-range missiles for use in highly maneuverable air combat with passive infrared allangles homing (Dual Band IHS) launch range: max, km - 40 minimum, km - 0.3 the height of the target, km - 0.02-20 overload of the target, g - up to 12 angles targeting - ± 60 ° angles for homing head - ± 75 ° starting weight, kg - 106 Warhead weight, kg - 8 length, m - 2.92 Diameter, m - 0.17 wingspan, m - 0.51 the scope of the rudders, m - 0,385 from manufacturer site: http://vympelmkb.com/products/prod01/ in russian keep in mind that article 810(RVV-BD) and R-37 is different thing, 810 for almost 100 kg lighter and shorter than R-37 to fit into PAK-FA bays , R-37 is missile for Mig-31BM KS-172 is canceled, this missile do not fit in PAK-FA bays and VVS dont want it on external,"Novator" wait for decision about new interceptor for second attempt
< Message edited by emsoy -- 6/6/2015 7:05:35 PM >
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