[PARTICLESTREAM_1]
NAME=engine1
SRCSIZE=0.5
SRCRATE=700
V0=100.0
SRCSPREAD=0.01
LIFETIME=0.055
GROWTHRATE=1.9
ATMSLOWDOWN=1.0
LTYPE=DIFFUSE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=2
ATMSMAP=ATM_PLOG
AMIN=1e-4
AMAX=1
[CONFIG]
MESHNAME="K-SR-71A-v2"
SIZE=10
EMPTY_MASS=18000
FUEL_MASS=20000
MAIN_THRUST=2.5e5
RETRO_THRUST=1e3
ATTITUDE_THRUST=5e3
ISP=50000
TRIM=0.05
PMI=(15.5,22.1,7.7)
CW_Z_POS=0.09
CW_Z_NEG=0.09
CW_X=2.
CW_Y=1.4
CROSS_SECTION=(53.0,186.9,25.9)
COG=2.47
PITCH_MOMENT_SCALE=0.00005
BANK_MOMENT_SCALE=0.00005
ROT_DRAG=(1.5,1.5,1.5)
WING_ASPECT=0.7
WING_EFFECTIVENESS=2.5
LAND_PT1=(0,-2.8,9)
LAND_PT2=(-4,-2.8,-5)
LAND_PT3=(4,-2.8,-5)
MAIN_PSTREAM1=engine1
[SOUND]
MAIN_THRUST=Sound\Vessel\SR-71\SR-71.wav
RCS_THRUST_ATTACK=Sound\Vessel\roll.wav
RCS_THRUST_SUSTAIN=Sound\Vessel\roll.wav
[AERODYNAMICS]
; lift/drag attack point of the vertical airfoil
VAIRFOIL_ATTACK=(0,0,-0.5)
; wing chord length of the vertical airfoil
VAIRFOIL_CHORD=20
; wing area of the vertical airfoil
VAIRFOIL_AREA=270
; wing aspect ratio of the vertical airfoil
VAIRFOIL_ASPECT=2.266
; lift/drag attack point of the horizontal airfoil
HAIRFOIL_ATTACK=(0,0,-4)
; wing chord length of the horizontal airfoil
HAIRFOIL_CHORD=20
; wing area of the horizontal airfoil
HAIRFOIL_AREA=50
; wing aspect ratio of the horizontal airfoil
HAIRFOIL_ASPECT=1.5
; surface area of aileron
AILERON_AREA=5
; lift change of aileron
AILERON_LIFT=3.3
; lift/drag attack point of left aileron (right aileron deduced by x -> -x
AILERON_ATTACK=(7,-0.5,-15)
; surface area of elevator
AILERON_RIGHT_ANIM=3
; reference to animation sequence for the right aileron
AILERON_LEFT_ANIM=2
; surface area of elevator
ELEVATOR_AREA=6.7
; lift change of elevator
ELEVATOR_LIFT=3.0
; lift/drag attack point of elevator
ELEVATOR_ATTACK=(0,0,-15)
; reference to animation sequence of elevator
ELEVATOR_ANIM=1
; surface area of rudder
RUDDER_AREA=2
; lift change of rudder
RUDDER_LIFT=1.5
; lift/drag attack point of rudder
RUDDER_ATTACK=(0,3,-16)
; reference to animation sequence of rudder
RUDDER_ANIM=4
; speed brake maximum drag change
SPEEDBRAKE_DRAG=5
; speed brake drag attack point
SPEEDBRAKE_ATTACK=(0,7.5,-14);
[EX_MAIN_0]
OFF=(-4,-0.4,-13.3)
DIR=(0,0,-1)
LENGTH=8
WIDTH=0.5
[EX_MAIN_1]
OFF=(4,-0.4,-13.3)
DIR=(0,0,-1)
LENGTH=8
WIDTH=0.5
[ANIM_SEQ_0]
; landing gear
KEY=G
DURATION=6.7
[ANIM_SEQ_1]
; elevator
INIT_POS=0.5
[ANIM_SEQ_2]
; left aileron
INIT_POS=0.5
[ANIM_SEQ_3]
; right aileron
INIT_POS=0.5
[ANIM_SEQ_4]
; rudder
INIT_POS=0.5
[ANIM_COMP_0]
; front gear cover
SEQ=0
GROUPS=54
RANGE=(0.5,0.9)
ROT_PNT=(-0.40,-1,4.1)
ROT_AXIS=(0,0,1)
ANGLE=95
[ANIM_COMP_1]
; rear left gear cover
SEQ=0
GROUPS=55
RANGE=(0.5,0.9)
ROT_PNT=(-2.4,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=105
[ANIM_COMP_2]
; rear right gear cover
SEQ=0
GROUPS=56
RANGE=(0.5,0.9)
ROT_PNT=(2.4,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=-105
[ANIM_COMP_3]
; front gear
SEQ=0
GROUPS=0,1,2,3,4,5,6,7,71,72
RANGE=(0.1,0.5)
ROT_PNT=(0,-1.2,6.2)
ROT_AXIS=(1,0,0)
ANGLE=-100
[ANIM_COMP_4]
; rear right gear
SEQ=0
GROUPS=13,14,15,16,19,76,77,78
RANGE=(0.1,0.5)
ROT_PNT=(2.4,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=-91
[ANIM_COMP_5]
; rear left gear
SEQ=0
GROUPS=8,9,10,11,12,73,74,75
RANGE=(0.1,0.5)
ROT_PNT=(-2.4,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=91
[ANIM_COMP_6]
SEQ=1
GROUPS=28,29
ROT_PNT=(0,-0.3,-13.5)
ROT_AXIS=(1,0,0)
ANGLE=22
[ANIM_COMP_7]
SEQ=2
GROUPS=34,35,36,37
ROT_PNT=(-10,-0.4,-12.0)
ROT_AXIS=(1,0,0)
ANGLE=-20;
[ANIM_COMP_8]
SEQ=3
GROUPS=30,31,32,33
ROT_PNT=(10,-0.4,-12.0)
ROT_AXIS=(1,0,0)
ANGLE=20;
[ANIM_COMP_9]
; rear left middle gear cover
SEQ=0
GROUPS=57
RANGE=(0.5,0.9)
ROT_PNT=(-0.1,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=-80
[ANIM_COMP_10]
; rear right middle gear cover
SEQ=0
GROUPS=58
RANGE=(0.5,0.9)
ROT_PNT=(0.1,-0.7,-7)
ROT_AXIS=(0,0,1)
ANGLE=80
[ANIM_COMP_11]
; rear left gear strut
SEQ=0
GROUPS=17
RANGE=(0.1,0.5)
ROT_PNT=(-1.0,-0.5,-7)
ROT_AXIS=(0,0,1)
ANGLE=-30
[ANIM_COMP_12]
; rear right gear conrod
SEQ=0
GROUPS=19
RANGE=(0.5,0.7)
ROT_PNT=(1.5,-0.5,-7)
ROT_AXIS=(0,0,1)
ANGLE=88
[ANIM_COMP_13]
; rear right gear strut
SEQ=0
GROUPS=18
RANGE=(0.1,0.5)
ROT_PNT=(1.0,-0.5,-7)
ROT_AXIS=(0,0,1)
ANGLE=30
[ANIM_COMP_14]
; rear left gear conrod
SEQ=0
GROUPS=11
RANGE=(0.5,0.7)
ROT_PNT=(-1.5,-0.5,-7)
ROT_AXIS=(0,0,1)
ANGLE=-88
[ANIM_COMP_15]
SEQ=4
GROUPS=62,65
RANGE=(0,1)
ROT_PNT=(-3.6,2,-13.2);
ROT_AXIS=(0.143,0.975,-0.172);
ANGLE=-33;
[ANIM_COMP_16]
SEQ=4
GROUPS=63,66
RANGE=(0,1)
ROT_PNT=(3.6,2,-13.2)
ROT_AXIS=(-0.143,0.975,-0.172)
ANGLE=-33