bestwork1989, thaks... I will take a look.
gattispilot, how I can acess the log?? and follows the ini below: (I use a SLS original codes and replace by the models that I make... there are no need to adapters, so I erase these parts, but did not work anyway. Sorry for the possible newbie mistakes that must be in the codes below)
[MISC]
cog=30.500
GNC_Debug=0
Telemetry=0
Focus=0
Thrust_real_pos=0
Vertical_Angle=0.000
[TEXTURE_LIST]
TEX_1=Exhaust_atsme
[PARTICLESTREAM_1]
Name=vent
amin =0.150
amax =1.000
atmslowdown =3.000
growthrate =1.200
lifetime =4.500
lmax =0.500
lmin =0.000
srcrate =15.000
srcsize =0.400
v0 =1.000
ltype =EMISSIVE
atmsmap =ATM_FLAT
levelmap =LVL_PSQRT
tex =contrail
Srcspread=0.000
[PARTICLESTREAM_2]
NAME=mach
SRCSIZE=7.000
SRCRATE=120.000
V0=12.000
SRCSPREAD=0.000
LIFETIME=0.250
GROWTHRATE=6.000
ATMSLOWDOWN=0.000
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0.000
LMAX=4.000
ATMSMAP=ATM_FLAT
AMIN=0.600
AMAX=1.000
TEX=contrail4
[FX_VENT]
pstream=vent
off_1=(4.200,0.000,35.000)
dir_1=(1.000,0.000,0.000)
time_fin_1=-15.000
off_2=(0.000,4.200,15.000)
dir_2=(0.000,1.000,0.000)
time_fin_2=-25.000
[FX_MACH]
pstream=mach
mach_min=0.900
mach_max=1.100
off_1=(0.000,0.000,70.000)
off_2=(6.777,0.000,20.000)
off_3=(-6.777,0.000,20.000)
dir=(0.000,0.000,-1.000)
[STAGE_1]
Height=63.720
Diameter=8.400
EmptyMass=51944.392
FuelMass=1101259.734
Thrust=10898383.375
BurnTime=449.000
off=(0.000,0.000,4.700)
MeshName=Montenegro-1st-ST
eng_1=(0.,0,-32.408)
eng_diameter=2.700
PITCHTHRUST=56774532.400
YAWTHRUST=56774532.400
speed=(0.000,0.000,-10.000)
ENG_PSTREAM1=
battery=1.500
Reignitable=0
Eng_tex=
Eng_pstream2=
Eng_dir=(0.000,0.000,1.000)
Module=Stage
Rot_speed=(0.000,0.000,0.000)
[SEPARATION_12]
MeshName="SLS\interstage"
SEPARATION_DELAY=15.0
Diameter=8.4
Height=5.0
EmptyMass=5650.32
off=(0.,0.,42.1027)
[STAGE_2]
MeshName=Montenegro-2nd-ST
Diameter=8.400
Height=13.700
EmptyMass=13883.576
FuelMass=273420.730
Thrust=3921000.000
BurnTime=306.500
ignite_delay=10.000
off=(0.000,0.000,47.876)
eng_1=(0,-1.3499,-12.5)
eng_2=(1.264,0.687,-12.5)
eng_3=(-1.264,0.687,-12.5)
eng_diameter=2.700
PITCHTHRUST=4663990.000
YAWTHRUST=4663990.000
battery=5.000
ullage_thrust=100000.000
ullage_N=4
ullage_angle=-22.500
ullage_pos=(4.200,0.000,-10.700)
ullage_dir=(0.200,0.000,-1.000)
ullage_tex=Exhaust_atsme
ullage_length=5.000
ullage_diameter=1.000
ullage_anticipation=3.000
ullage_overlap=1.000
ullage_rectfactor=3.000
reignitable=1
Linearthrust=500000.000
Eng_tex=
Eng_pstream1=
Eng_pstream2=
Eng_dir=(0.000,0.000,1.000)
Module=Stage
Speed=(0.000,0.000,0.000)
Rot_speed=(0.000,0.000,0.000)
[FAIRING]
N=2
MeshName="Montenegro Nose RH"
Diameter=10
Height=31.35
angle=0.
off=(0,0.,73.695)
EMPTYMASS=10683.0145
speed=(25,0,0)
Rot_speed(0,0.3,0)
[PAYLOAD_1]
MeshName="SLS\deadweight"
off=(0,0,68.695)
Diameter=8
Height=20
MASS=130000
Module="spacecraft\spacecraft3"
Name=Deadweight
SPEED=(0,0,2)
RENDER=1
[PAYLOAD_2]
MeshName="SLS\adapter"
off=(0,0,58.695)
Diameter=8
Height=20
MASS=200
Module="spacecraft\spacecraft3"
Name=Adapter
SPEED=(0,0,2)
RENDER=1
[FX_LAUNCH]
N=2
Height=0.500
Angle=90.000
Distance=10.000
CutoffAltitude=150.000
Pstream1=flametrench
Pstream2=
[PARTICLESTREAM_3]
Name=flametrench
Srcsize=11.000
Srcrate=15.000
V0=100.000
Srcspread=0.000
Lifetime=10.000
Growthrate=15.000
Atmslowdown=0.500
Ltype=EMISSIVE
Levelmap=LVL_PSQRT
Lmin=0.000
Lmax=0.500
Atmsmap=ATM_FLAT
Amin=1.000
Amax=1.000
Tex=contrail
The "Montenegro" rocket that appears in some codes have the respective meshes.
So I have the Ini codes and the meshes. Is there anything else besides that i'm missing?
Thanks!
