;LATE MODEL


acceleration factor = 300.0

;rev ratio = {1.95, 1.0, 1.0, 1.0, 2.9}
rev ratio = {1.25, 0.85, 0.85, 0.85, 5.2}

;tyre width = {0.813,1.05}
tyre width = {0.813,1.075}

;tyre width = {0.74,0.973}
;tyre width = {0.84,1.073}

wheel inertia = 6.453

centre of gravity = {0.0, -2.123454, 1.9}

wheelbase front = {3.52532,-2.10704,8.21492}
wheelbase back = {3.55632,-2.45704,-4.53113}
wheel radii = {1.65907,1.70907}

wing pos = {0.0, 3.5, 1.0}
side wing angle = 0.0
;side wing size = 0.03
side wing size = 0.01
top wing angle = 0.35
top wing size = 0.015
;top wing size = 0.0
static weight = 0.5

max travel fl = 1.0
max travel fr = 1.0
max travel rl = 0.9
max travel rr = 1.1

; roof points relative to COG
nodefbody = 1

roof front = {2.232251, -0.304062, 7.9}
;roof front = {0.1, 4.2, -0.1}
roof back = {2.232251, 1.0, -8.6}
body base 0 = {0.000000, 0.9, 0.0}

roof front radius = 2.258436
roof back radius = 2.453498
body radius = 2.5

cockpit = {0.000000, 1.72, -1.890117}

core base = {0.0, 0.567, 0.70883}

num exhausts = 2
exhaust1 = {-2.0, -1.1, -9.8}
exhaust2 = {-2.1, -1.2, -9.8}
exhaust high rpm = 6000.0
exhaust low rpm  = 4750.0
exhaust high to low time needed = 60

; For optimised mesh loading
; Submeshes are wheels x 4, alpha, driver
submeshes in top lod = 6
