Hi Jacques,
yes - I remember making the "ELS-Arms" with Papyref! Well done for renovating the Kourou CSG :thumbup:
Thanks for your suggestion - I have a "workaround" now (I attach the "MS_Launchpad" to my "SLC17" vessel).
@Fred18
Hi Fred,
I can't use the "Pad_module = xxx" in the .ini file because the pad is created in the wrong attitude (+Z axis = Vertical) and I need (+Y axis = Vertical).
The attitude can be edited in a saved scenario but the attachment point is always created in the wrong attitude (launcher is horizontal) and wrong position.
Also, there are 2 pads at my SLC17 add-on (Pad A and Pad B) - each of these has it's own attachment point for the launcher.
So, I have created a simple .cfg based vessel for the "MS_Launchpad" and this is already attached to my SLC17 launchpad(at Pad A or Pad B) in the scenario. The launcher is attached to "MS_Launchpad" vessel.
This works, but it might be useful to have the possibility to disable the MS_Launchpad creation and attachment functions.
I have a couple of other issues I should mention:
1. If the scenario is exited during ascent(autopilot is running), when the scenario is re-started the launcher rolls 90deg left (Prograde attitude) instead of "Heads Up" or "Heads Down" - is this expected?
2. Burndelay=xxx parameter
When the DeltaII has 9 SRB's(3 sets of 3 each). The first 6 are jettisoned at burnout(about 63s after liftoff) and the final 3 are ignited at that time.
I am using Burndelay=63 for the final set of 3 SRB's but they do not ignite at T+63s, more like T+78s.
If I change the Burndelay value the results seem "variable" e.g if Burndelay=48 the ignition starts at ~ T+48s
I am still looking at this, but I can't seem to get the final 3 SRB's to ignite at the correct time.
Here are my launcher .ini and guidance file:
.ini file
guidance file:
As always, many thanks for your great work with MS
Cheers,
Brian
yes - I remember making the "ELS-Arms" with Papyref! Well done for renovating the Kourou CSG :thumbup:
Thanks for your suggestion - I have a "workaround" now (I attach the "MS_Launchpad" to my "SLC17" vessel).
@Fred18
Hi Fred,
I can't use the "Pad_module = xxx" in the .ini file because the pad is created in the wrong attitude (+Z axis = Vertical) and I need (+Y axis = Vertical).
The attitude can be edited in a saved scenario but the attachment point is always created in the wrong attitude (launcher is horizontal) and wrong position.
Also, there are 2 pads at my SLC17 add-on (Pad A and Pad B) - each of these has it's own attachment point for the launcher.
So, I have created a simple .cfg based vessel for the "MS_Launchpad" and this is already attached to my SLC17 launchpad(at Pad A or Pad B) in the scenario. The launcher is attached to "MS_Launchpad" vessel.
This works, but it might be useful to have the possibility to disable the MS_Launchpad creation and attachment functions.
I have a couple of other issues I should mention:
1. If the scenario is exited during ascent(autopilot is running), when the scenario is re-started the launcher rolls 90deg left (Prograde attitude) instead of "Heads Up" or "Heads Down" - is this expected?
2. Burndelay=xxx parameter
When the DeltaII has 9 SRB's(3 sets of 3 each). The first 6 are jettisoned at burnout(about 63s after liftoff) and the final 3 are ignited at that time.
I am using Burndelay=63 for the final set of 3 SRB's but they do not ignite at T+63s, more like T+78s.
If I change the Burndelay value the results seem "variable" e.g if Burndelay=48 the ignition starts at ~ T+48s
I am still looking at this, but I can't seem to get the final 3 SRB's to ignite at the correct time.
Here are my launcher .ini and guidance file:
.ini file
Code:
[MISC]
cog=-1.2
[TEXTURE_LIST]
TEX_1=Exhaust2
[PARTICLESTREAM_1]
NAME=Delta311contrail
SRCSIZE=1.1
SRCRATE=4
V0=125
SRCSPREAD=0.1
LIFETIME=2
GROWTHRATE=7
ATMSLOWDOWN=1.1
LTYPE=DIFFUSE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=1
ATMSMAP=ATM_PLOG
AMIN=1e-5
AMAX=1
TEX=contrail1
[PARTICLESTREAM_2]
NAME=Delta311contrail2
SRCSIZE=3.0
SRCRATE=4
V0=160
SRCSPREAD=0.02
LIFETIME=0.3
GROWTHRATE=10
ATMSLOWDOWN=0.4
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=1
ATMSMAP=ATM_PLOG
AMIN=1e-5
AMAX=1
TEX=contrail3
[PARTICLESTREAM_3]
NAME=Delta311contrail3
SRCSIZE=4.0
SRCRATE=15
V0=120.0
SRCSPREAD=0.05
LIFETIME=0.15
GROWTHRATE=0.8
ATMSLOWDOWN=0
LTYPE=EMISSIVE
LEVELMAP=LVL_PSQRT
LMIN=0
LMAX=1
ATMSMAP=ATM_PLOG
AMIN=1e-5
AMAX=1
TEX=contrail3
[BOOSTER_1]
N=3
MeshName="Delta2/gem40"
Height=12.96
Diameter=1.02
EmptyMass=1317
FuelMass=11765
Thrust=490320
angle=0
off=(1.7,0.0,-7.4)
rot_speed=(0,-2,0)
speed=(8,0,0)
BurnTime=61.3
ENG_TEX=Exhaust2
eng_1=(0,0,-7.3)
eng_diameter=0.75
ENG_PSTREAM1=Delta311contrail
ENG_PSTREAM2=Delta311contrail2
CURVE_1=(0,91.3)
CURVE_2=(62,100)
[BOOSTER_2]
N=3
MeshName="Delta2/gem40a"
Height=12.96
Diameter=1.02
EmptyMass=1317
FuelMass=11765
Thrust=490320
angle=40
off=(1.7,0.0,-7.4)
rot_speed=(0,-2,0)
speed=(8,0,0)
BurnTime=62.3
ENG_TEX=Exhaust2
eng_1=(0,0,-7.3)
eng_diameter=0.75
ENG_PSTREAM1=Delta311contrail
ENG_PSTREAM2=Delta311contrail2
CURVE_1=(0,91.3)
CURVE_2=(62,100)
[BOOSTER_3]
N=3
Burndelay=63
MeshName="Delta2/gem40b"
Height=12.96
Diameter=1.02
EmptyMass=1439
FuelMass=11765
Thrust=490320 ;516216?
angle=80
off=(1.7,0.0,-7.4)
rot_speed=(0,-0.5,0)
speed=(5,0,0)
BurnTime=62.5
ENG_TEX=Exhaust2
eng_1=(0,0,-7.3)
eng_diameter=0.75
ENG_PSTREAM1=Delta311contrail
ENG_PSTREAM2=Delta311contrail2
[STAGE_1]
Height=30.77
Diameter=2.44
EmptyMass=5678
FuelMass=96118
Thrust=1085811
BurnTime=261
off=(0,0,0)
MeshName="Delta2/delta2core"
ENG_TEX=Exhaust2
ENG_1=(0,0,-16)
ENG_DIAMETER=1
ENG_PSTREAM1=Delta311contrail3
speed=(0,0,-2)
rot_speed=(0,0,0)
PITCHTHRUST=100000
YAWTHRUST=100000
ROLLTHRUST=30000
[STAGE_2]
Height=5.89
Diameter=2.44
EmptyMass=950
FuelMass=6004
Thrust=44996 ;43657
BurnTime=431.6
off=(0,0,14.8)
MeshName="Delta2/delta2stg2"
ENG_1=(0,0,-3)
ENG_DIAMETER=0.6
ENG_TEX=Exhaust2
IGNITE_DELAY=13.5
PITCHTHRUST=5300
YAWTHRUST=5300
ROLLTHRUST=5300
speed=(0,0,-2)
rot_speed=(0.01,0,0)
[STAGE_3]
Height=1.68
Diameter=0.93
EmptyMass=208
FuelMass=2009
Thrust=66367
BurnTime=87 ;87.1
OFF=(0,0,18.4)
MeshName="Delta2/star_48b"
ENG_1=(0,0,-1.1)
ENG_DIAMETER=0.3
ENG_TEX=Exhaust2
IGNITE_DELAY=82
PITCHTHRUST=2000
YAWTHRUST=2000
ROLLTHRUST=1000
speed=(0,0,-1)
rot_speed=(0.1,0,0)
[FAIRING]
N=2
MeshName="Delta2/delta2fair9"
Diameter=2.9
Height=8.49
angle=0
off=(0,0,19.8)
speed=(3,0,0)
rot_speed=(0,-0.5,0)
EMPTYMASS=839
[PAYLOAD_1]
MeshName=Delta2/test_sat
OFF=(0,0,20.3)
speed=(0,0,0.5)
rot_speed=(0,0,0)
Module="Delta2/test_sat"
name="TestSat"
Diameter=2
Height=3
Mass=500
guidance file:
Code:
-3=engine(0,100,3)
0=engine(100,100,1)
7=roll(3,88,99.3,69,1)
26=pitch(69,57,14)
40=pitch(57,50,10)
47=engine(100,85,3)
50=engine(85,85,1)
50=pitch(50,44,10)
60=pitch(44,39,10)
70=pitch(39,34,10)
75=engine(85,100,5)
80=pitch(34,30.5,10)
80=engine(100,100,1)
90=pitch(30.5,26.5,10)
100=pitch(26.5,23.5,10)
110=pitch(23.5,20.7,10)
120=pitch(20.7,19,10)
130=pitch(19,16,10)
140=pitch(16,13,10)
150=pitch(13,10,10)
160=pitch(10,5,10)
170=pitch(5,5,10)
180=pitch(5,5,10)
190=pitch(5,5,10)
200=pitch(5,5,20)
220=pitch(5,27,15)
235=pitch(27,27,10)
245=pitch(27,5,15)
260=pitch(5,5,25)
285=pitch(5,3,5)
290=pitch(3,2.3,280)
296=fairing()
567=engine(100,0,1.5)
568.5=engine(0,0,1)
570=pitch(2.3,0,10)
580=aoa(0)
1512=pitch(0,10,10)
1522=pitch(10,10,100)
1528=engine(0,100,1)
1529=engine(100,100,1)
1622=pitch(10,3,7)
1629=aoa(0)
1635=engine(100,0,1)
1636=engine(0,0,1)
1652=jettison() ; 3rd stage
1662=aoa(5)
1852=jettison() ; spacecraft separation
As always, many thanks for your great work with MS
Cheers,
Brian