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OFMM-1 - Communications satellite to Lunar Orbit
The scenario:
The custom INI file for the DSCS satellite
This file MUST be named OFMM-1.ini and placed in the [ORBITER]\config\nep-1 folder.
Required Add-ons:
[ame="http://www.orbithangar.com/searchid.php?ID=3666"]Wideawake[/ame]
[ame="http://www.orbithangar.com/searchid.php?ID=4693"]Neptune-1[/ame]
Multistage-2
Spacecraft3
[ame="http://www.orbithangar.com/searchid.php?ID=4661"]stage.dll[/ame]
[ame="http://www.orbithangar.com/searchid.php?ID=5517"]DCS02[/ame]
NOTE: No add on MFD for Earth - Moon has been suggested. It is the mission commanders DECISION to use whichever they feel comfortable with. The commander has sole discretion on how the mission is executed. Any deviations from the flight plan should be noted in a post mission report.
Enjoy!
The scenario:
BEGIN_DESC
OFMM-1 - This mission will take the NASA DSCS satellite delivered in OFMM-P1 and launch it on a Neptune-1 Rocket into Lunar orbit for two weeks of Earth - DSCS testing. At the end of the two week period the DSCS should be left in a 600 x 660km lunar orbit and in hibernation should it be required during the Mars missions.
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 55998.7218253052
END_ENVIRONMENT
BEGIN_SHIPS
Nep-1:Multistage\Multistage2
STATUS Landed Earth
POS -14.4367100 -7.9794500
HEADING 90.00
AFCMODE 7
PRPLEVEL 0:1.000000 1:1.000000 2:1.000000 3:1.000000 4:1.000000
NAVFREQ 0 0
CONFIG_FILE Config\Nep-1\OFMM-1.ini
GUIDANCE_FILE Config\Nep-1\guidance_nep-1.txt
CONFIGURATION 0
STAGE_STATE 2
STAGE_IGNITION_TIME 0.000000
CURRENT_BOOSTER 1
CURRENT_STAGE 1
CURRENT_INTERSTAGE 1
CURRENT_PAYLOAD 1
FAIRING 1
END
END_SHIPS
The custom INI file for the DSCS satellite
Code:
MISC]
cog=20
GNC_DEBUG=1
FOCUS=1
[TEXTURE_LIST]
TEX_1=Nep-1\exhaust
TEX_2=Nep-1\Ncontrail1
TEX_3=Nep-1\Ncontrail2
TEX_4=Nep-1\Explosivebolt
TEX_5=Nep-1\UDMHexhaust
[PARTICLESTREAM_1]
NAME=con1
SRCSIZE=1.8
SRCRATE=1000
V0=130.0
SRCSPREAD=0
LIFETIME=0.1
GROWTHRATE=-4
ATMSLOWDOWN=2.0
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=0
ATMSMAP=ATM_PLOG
AMIN=0.7e-7
AMAX=1
TEX=Nep-1\Ncontrail1
[PARTICLESTREAM_2]
NAME=con2
TEX=Nep-1\Ncontrail2
SRCSIZE=1.6
SRCRATE=150
V0=110.0
SRCSPREAD=0.1
LIFETIME=4
GROWTHRATE=14
ATMSLOWDOWN=1.0
LTYPE=DIFFUSE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=1
ATMSMAP=ATM_PLOG
AMIN=1e-4
AMAX=2
[PARTICLESTREAM_3]
NAME=con3
TEX=Nep-1\Ncontrail2
SRCSIZE=1.9
SRCRATE=1100.0
V0=110.0
SRCSPREAD=0.05
LIFETIME=0.40
GROWTHRATE=14
ATMSLOWDOWN=0.0
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=0
ATMSMAP=ATM_PLOG
AMIN=0.7e-7
AMAX=1
[PARTICLESTREAM_4]
NAME=maxq
SRCSIZE=5
SRCRATE=120
V0=12
SRCSPREAD=0
LIFETIME=0.18
GROWTHRATE=6
ATMSLOWDOWN=0
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=4
ATMSMAP=ATM_PLOG
AMIN=0.7e-7
AMAX=1
TEX=Nep-1\Ncontrail1
[PARTICLESTREAM_5]
NAME=explosivebolt
SRCSIZE=3
SRCRATE=500
V0=90.0
SRCSPREAD=0.05
LIFETIME=0.15
GROWTHRATE=40
ATMSLOWDOWN=0
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=2
ATMSMAP=ATM_PLIN
AMIN=-1
AMAX=1
TEX=Nep-1\Explosivebolt
[BOOSTER_1]
N=1
MeshName="Nep-1\bolt1"
Height=1
Diameter=1
EmptyMass=0.001
FuelMass=0.001
Thrust=0.00001
angle=0
off=(0,0,0)
eng_1=(0,0,54.5)
eng_diameter=0
Burndelay=55
BurnTime=10
ENG_PSTREAM1=maxq
Rot_Speed=(0,0,0)
speed=(0,0,-30)
[BOOSTER_2]
N=1
MeshName="Nep-1\bolt2"
Height=1
Diameter=1
EmptyMass=0.001
FuelMass=0.001
Thrust=0.00001
angle=0
off=(0,0,0)
eng_1=(-1.662,1.662,39.23)
eng_2=(-1.662,-1.662,39.23)
eng_3=(1.662,-1.662,39.23)
eng_4=(1.662,1.662,39.23)
eng_diameter=0
Burndelay=146
BurnTime=1
ENG_PSTREAM1=explosivebolt
Rot_Speed=(0,0,0)
speed=(0,0,-30)
[STAGE_1]
Height=40
Diameter=10
EmptyMass=55420
FuelMass=477745
Thrust=8896250
BurnTime=145
off=(0.,0.,19.628)
eng_1=(0,0,-19.628)
eng_diameter=2.2
ENG_TEX=Nep-1\exhaust
ENG_PSTREAM1=con2
ENG_PSTREAM2=con3
MeshName="Nep-1\Ns1"
SPEED=(0,0,-3)
ROT_SPEED=0
[SEPARATION_12]
Height=4.6
Diameter=5
Emptymass=1500
MeshName="Nep-1\Nint"
OFF=(0,0,41.528)
ROT_SPEED=0
SEPARATION_DELAY=15
[STAGE_2]
Height=12
Diameter=5
EmptyMass=3848
FuelMass=77980
Thrust=822000
BurnTime=319
off=(0.,0.,44.615)
MeshName="Nep-1\Ns2"
eng_1=(1,0,-4.87)
eng_2=(-1,0,-4.87)
eng_diameter=0.95
ENG_TEX=Nep-1\exhaust
ENG_PSTREAM1=con1
SPEED=(0,0,-3)
ROT_SPEED=0
[STAGE_3]
;Fregat Space Tug
Height=4
Diameter=4
EmptyMass=1100
FuelMass=5435
Thrust=19600
Pitchthrust=19600
Yawthrust=19600
BurnTime=889
off=(0.,0.,50.308)
MeshName="Nep-1\Fregat"
eng_1=(0,0,-1)
eng_diameter=0.35
ENG_TEX=Nep-1\UDMHexhaust
SPEED=(0,0,-2)
ROT_SPEED=0
[FAIRING]
N=2
MeshName="Nep-1\Nf1L"
Diameter=6
Height=23
angle=0
off=(1.391,0,54.16)
SPEED=(4.6,0.0,1.8)
ROT_SPEED=(0.0,-12,0.0)
emptymass=3210
[PAYLOAD_1]
off=(0,0,53.187)
speed=(0,0,1.0)
rot_speed=(0,0,0)
MeshName="DSCS"
Module="spacecraft\spacecraft3"
name="DSCS"
Diameter=4
Height=8
Mass=1600
This file MUST be named OFMM-1.ini and placed in the [ORBITER]\config\nep-1 folder.
Required Add-ons:
[ame="http://www.orbithangar.com/searchid.php?ID=3666"]Wideawake[/ame]
[ame="http://www.orbithangar.com/searchid.php?ID=4693"]Neptune-1[/ame]
Multistage-2
Spacecraft3
[ame="http://www.orbithangar.com/searchid.php?ID=4661"]stage.dll[/ame]
[ame="http://www.orbithangar.com/searchid.php?ID=5517"]DCS02[/ame]
NOTE: No add on MFD for Earth - Moon has been suggested. It is the mission commanders DECISION to use whichever they feel comfortable with. The commander has sole discretion on how the mission is executed. Any deviations from the flight plan should be noted in a post mission report.
Enjoy!