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Crusader

+MODDER
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Everything posted by Crusader

  1. Crusader

    img00161.JPG

    From the album: CrusaderScreens

  2. Reminds me of ThirdWire's First Flight: The Wright Experience Flight Simulator http://www.simhq.com/_air/air_076a.html Probably hard to find now...
  3. Ah.. ok, sorry. I've not seen that the file is in that place.
  4. I do not have the error msg.
  5. https://combatace.com/files/file/14969-btr-407z/
  6. Found this max file while looking for something else
  7. Interesting fuselage pylon. FAA mod ?
  8. Welcome Replayability - enormous. Each single player and campaign mission is created dynamically. Even if you happen to fail a mission and choose to replay it - there can be additional or less enemy flights etc, different SAM types. Very dynamic. Also depends on your difficult settings.
  9. But of course. We've released the CK long ago (not up to date anymore) and have an updated CK and the CK2 on the assembly line.
  10. Shells ejection position update can be added to the new UB as well. The UB has a reduced ammo capacity, only 50 rounds. Its mentioned in one of the manuals, IIRC.
  11. From the archives... Shells ejection update for TMF MiG-29A and S // Internal Guns --------------------------------------------------------- [InternalGun] ... EjectShells=TRUE EjectPosition=-0.350,1.00,0.130 EjectVelocity=1.0,0.0,-9.0 ...
  12. I too experience the upload problem. On PC when using PMs. Wont upload files bigger than (approx.) 1 mb if they are dragged into the message window. It does work OK if I attach the file by using the 'chose files' option.
  13. web-archive link to IPMSSA Impala article Pages 1 to 3 cover MkI, pages 4-5 MkII MkII serials, the first was 1000 .. with 100 ac to 1099
  14. Use mouse cursor and backspace to re-align the entries and offset line spaces... or simply copy/paste my fixed RightOuterWing section over the faulty section [RightOuterWing] ParentComponentName=RightWing ModelNodeName= ShowFromCockpit=TRUE DetachWhenDestroyed=TRUE DamageRating=DISABLED MassFraction=0.066 HasAeroCoefficients=TRUE LiftSurface=TRUE CL0=0.0330 CLa=1.1675 CD0=0.0009 CDL=0.0052 Cmq=-0.0151 Cmad=0.5244 Cyb=-0.0038 Clb=-0.0184 Clp=-0.1596 Clr=0.0160 Cnp=-0.0021 Cnr=-0.0413 CL0MachTableNumData=11 CL0MachTableDeltaX=0.10 CL0MachTableStartX=0.00 CL0MachTableData=0.927,0.931,0.944,0.966,1.000,1.049,1.118,1.219,1.373,1.633,2.029 CLaMachTableNumData=11 CLaMachTableDeltaX=0.10 CLaMachTableStartX=0.00 CLaMachTableData=0.927,0.931,0.944,0.966,1.000,1.049,1.118,1.219,1.373,1.633,2.029 CD0MachTableNumData=11 CD0MachTableDeltaX=0.10 CD0MachTableStartX=0.00 CD0MachTableData=2.106,1.246,1.092,1.031,1.000,0.978,0.957,0.972,0.993,1.045,9.549 CDLAlphaTableNumData=15 CDLAlphaTableDeltaX=4.00 CDLAlphaTableStartX=-28.00 CDLAlphaTableData=22.014,15.844,10.686,6.541,3.408,1.287,0.179,0.083,1.000,2.929,5.871,9.825,14.791,20.770,27.762 CmqMachTableNumData=11 CmqMachTableDeltaX=0.10 CmqMachTableStartX=0.00 CmqMachTableData=0.832,0.837,0.869,0.919,1.000,1.127,1.333,1.696,2.460,4.888,22.222 ClbAlphaTableNumData=37 ClbAlphaTableDeltaX=10.00 ClbAlphaTableStartX=-180.00 ClbAlphaTableData=1.205,1.241,1.345,1.506,1.702,1.912,2.108,2.268,2.373,2.205,1.970,1.883,1.750,1.587,1.413,1.250,1.117,1.030,1.000,4.000,6.000,7.765,6.824,7.765,6.353,3.647,6.118,4.409,3.577,2.870,2.108,1.912,1.702,1.506,1.345,1.241,1.205 CnrAlphaTableNumData=37 CnrAlphaTableDeltaX=10.00 CnrAlphaTableStartX=-180.00 CnrAlphaTableData=0.000,0.004,0.015,0.034,0.060,0.094,0.134,0.181,0.234,0.293,0.357,0.426,0.500,0.577,0.658,0.741,0.826,0.913,1.000,0.913,0.826,0.741,0.658,0.577,0.500,0.426,0.357,0.293,0.234,0.181,0.134,0.094,0.060,0.034,0.015,0.004,0.000 XacMachTableNumData=11 XacMachTableDeltaX=0.10 XacMachTableStartX=0.00 XacMachTableData=0.098,0.098,0.097,0.095,0.092,0.089,0.086,0.082,0.092,0.109,0.149 CheckStall=TRUE CLmax=0.3012 AlphaStall=11.05 AlphaMax=16.45 AlphaDepart=20.45 StallMoment=-0.000 StallDrag=0.001 StallLiftTableNumData=37 StallLiftTableDeltaX=10.00 StallLiftTableStartX=-180.00 StallLiftTableData=0.000,-0.012,-0.026,-0.042,-0.057,-0.053,-0.046,-0.031,-0.013,0.000,0.017,0.049,0.093,0.138,0.200,0.241,0.336,0.524,0.891,0.578,0.357,0.261,0.208,0.165,0.117,0.073,0.037,0.000,-0.013,-0.031,-0.046,-0.053,-0.057,-0.042,-0.026,-0.012,0.000 StallDragTableNumData=37 StallDragTableDeltaX=10.00 StallDragTableStartX=-180.00 StallDragTableData=0.001,0.008,0.021,0.043,0.082,0.123,0.171,0.227,0.292,0.367,0.451,0.562,0.689,0.825,0.937,1.018,1.142,1.122,1.000,1.122,1.142,1.018,0.937,0.825,0.689,0.562,0.451,0.367,0.292,0.227,0.171,0.123,0.082,0.043,0.021,0.008,0.001 StallXacShiftTableNumData=37 StallXacShiftTableDeltaX=10.00 StallXacShiftTableStartX=-180.00 StallXacShiftTableData=-0.580,-0.580,-0.496,-0.446,-0.441,-0.424,-0.394,-0.363,-0.321,-0.290,-0.259,-0.217,-0.186,-0.156,-0.139,-0.134,-0.084,0.000,0.000,0.000,-0.084,-0.134,-0.139,-0.156,-0.186,-0.217,-0.259,-0.290,-0.321,-0.363,-0.394,-0.424,-0.441,-0.446,-0.496,-0.580,-0.580 Chord=1.55 Ymac=4.61 MinExtentPosition= MaxExtentPosition= CollisionPoint[001]= CollisionPoint[002]= HasVortexEmitter=TRUE VortexEmitterName=WingtipVortexEmitter VortexPosition= 4.755,-1.09, 0.22 VortexG=2.5 SystemName[001]=RightAileron SystemName[002]=RightPositionLight HasArmor=TRUE ArmorMaterial=Aluminium Armor[TOP].Thickness=2 Armor[BOTTOM].Thickness=2 Another small typo fix [RightWingFuelCell] ... MinExtentPosition=4.40,-3.70,-0.07 should be MinExtentPosition=4.40,-3.07,-0.07
  15. RightOuterWing section has faulty lines, that disables the right aileron/vortex/navlight
  16. New loadout image ImpalaMkII_Loadout.zip - change file extension to TGA in ImpalaMkII ini - to make the pylons on the image line up with the station lines, change ReferenceSpan to 9.4 in data ini Thats the actual size of the lod.. a bit short of the real size
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