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Show new changes starting from 06:50, 19 January 2020
   
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18 January 2020

     20:49  MiG-21SMT‎‎ (6 changes | history) . . (+1,169). . [ZdrytchX‎ (6×)]
 m    20:49 (cur | prev) . . (+56). . ZdrytchX (talk | contribs) (MiG-21 is a suprisingly good glider) (Tag: Visual edit)
      20:40 (cur | prev) . . (+6). . ZdrytchX (talk | contribs) (Details) (Tag: Visual edit)
 m    20:32 (cur | prev) . . (+43). . ZdrytchX (talk | contribs) (more gun information) (Tag: Visual edit)
 m    20:17 (cur | prev) . . (+429). . ZdrytchX (talk | contribs) (Corner speed from 2 tests, new calculations. Note that G-overload broundy is a probability zone so may very likely be below the actual recorded number. I'm too tired to test anymore) (Tag: Visual edit)
      19:22 (cur | prev) . . (+545). . ZdrytchX (talk | contribs) (An entire section for wing performance statistics tested freshly by myself. Best IAS climb speeds are rough estimates within ~5% with mathematical extrapolation only. Glide spds are apprx within ~2%.) (Tag: Visual edit)
      18:38 (cur | prev) . . (+90). . ZdrytchX (talk | contribs) (Tested 1300kph limit + ~450kph estimate gear limit. Also note that while it is reasonably safe to linger above the redline at 1320kph for 5 seconds in the F-13, the SMT will likely breakup after only 1 second.) (Tag: Visual edit)
     19:48  MiG-21F-13‎‎ (6 changes | history) . . (-95). . [ZdrytchX‎ (6×)]
      19:48 (cur | prev) . . (-105). . ZdrytchX (talk | contribs) (Formally tested maximum stall speed range. It seems that fuel load difference was a lie. Also updated thrust based on what it should be based on bug reports + maximum thrust tested on deck of 5480kgf (should be 5900 but w/e gaijin likely uses 1.4x still)) (Tag: Visual edit)
 m    19:24 (cur | prev) . . (-5). . ZdrytchX (talk | contribs) (Remove duplicate altitude information (wiki bug? sometimes it appears sometimes it doesnt)) (Tag: Visual edit)
      18:56 (cur | prev) . . (-4). . ZdrytchX (talk | contribs) (No combat/take-off setting) (Tag: Visual edit)
      18:33 (cur | prev) . . (+15). . ZdrytchX (talk | contribs) (Added stat card statistics + gear speed limit ~250 knots ~450 kph and confirmed redline limit.) (Tag: Visual edit)
      18:28 (cur | prev) . . (+16). . ZdrytchX (talk | contribs) (1.95 added my "fix" but the afterburner multiplier is as expected ~5490 instead of the IRL 5900 presumably because gaijin is still using the 1.4 multiplier from the 3900kgf static thrust (to be tested but presumably so)) (Tag: Visual edit)
 m    18:25 (cur | prev) . . (-12). . ZdrytchX (talk | contribs) (-G-load dependance (confirmed wing loading variable). May need recalculations.) (Tag: Visual edit)

17 January 2020

     01:01 (Revision approval log) . . Kmsxkuse (talk | contribs) set 41930 as the approved revision for "He 162 A-2" ‎

16 January 2020

     18:12  He 162 A-2‎ (diff | hist) . . (0). . AlienX82 (talk | contribs) (i provided minor change of one con) (Tag: Visual edit)

13 January 2020

     07:21 (Revision approval log) . . Inceptor57 (talk | contribs) set 41744 as the approved revision for "He 162 A-2" ‎

12 January 2020

     21:08  He 162 A-2‎ (diff | hist) . . (-61). . AlienX82 (talk | contribs) (i provided minor corrections to describe this plane better) (Tag: Visual edit)