4
Tomahawk Starfighter
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Lester Anderson
Version 2. Version 1 was deleted the last time my hard drive crashed in my computer.
4
61
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0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
1.06584
49.2963
0.00371577
0.00371577
0.
0
0.
0.261799
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
23
0
0
2
blue
2.89346
0.179792
9.1533
0.184337
1
0
8
0
152.4
1
101.6
28.02
25.4
28.7554
23.31
1.5875
2
0
0
0.
0.
0.
1
0.
0.
33.5296
12.9447
0.275787
0.
0.
57.26
28.0209
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
1.06584
49.2963
0.00371577
0.00371577
0.
0
0.
0.523599
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
24
0
0
2
blue
2.89346
0.179792
11.2105
0.184337
1
0
8
0
152.4
1
101.6
28.02
25.4
28.7554
23.31
1.5875
2
0
0
0.
0.
0.
1
0.
0.
33.5296
12.9447
0.275787
0.
0.
57.26
28.0209
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
798.85
afterburner rear
0.
0
365.76
32.8245
22.2473
0.00530446
0.00530446
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
rgb(206,211,255)
white
1
18
0
0
0
blue
-3.21248
0.226667
-3.21248
0.226667
1
0
8
0
203.2
40.386
25.3746
50.8
0
0.
0.
1
12.7
0.
0.
0.
0
0.
136.674
85.8738
Custom
0.
337.541
1/8 Aircraft Plywood
Right body plate
0.
0
-50.8
6.20613
93.3144
0.0103226
0.0103226
0.
0
0.
-1.5708
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
43
1
0
0
blue
2.77733
-7.10543e-18
6.54082
0.
1
0
8
0
-50.8
1
203.2
203.2
25.4
25.4
0.
3.175
2
3
0
50.8
12.3952
0.
1
0.
0.
25.0952
7.55269
1.
0.
0.
203.2
203.2
203.2,0|203.2,25.4|0,25.4|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
0.
engine mount.
Engine mount.
0.
0
-111.76
0.
0.
0.
0.
0.
0
57.9882
-1.5708
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
44
1
0
0
blue
0.
0.
0.
0.
1
0
8
0
-162.56
0
1
1
Semroc
1.09996
128.148
Balsa
Nose cone
25.4
1
0.
3.82746
122.943
0.00719025
0.00719025
0.
0
BC-15044
Conical nose cone
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
rgb(206,211,255)
white
1
45
1
0
0
rgb(0,0,0)
2.
-0.0881278
2.
-0.0881278
1
0
8
0
-162.56
111.76
40.386
1
0
0
25.4
0.127
0.
38.1
0.
0.
0.
Estes
155.922
0.
Estes
lead weight
101.6
1
101.6
0.
0.
0.
0.
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
46
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
-60.96
0
0.
Semroc
0.
848.979
Spiral/Glassine
Engine tube
0.
0
111.76
24.3097
101.6
0.0257813
0.0257813
0.
0
LT-150300
Large Body Tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
47
1
0
0
blue
0.
0.
0.
0.
1
0
8
0
-50.8
40.386
38.1
203.2
0
0
0.
0.5
0.
0.
0
0
Semroc
0.
848.979
Spiral/Glassine
Body tube
0.
0
-101.6
7.15181
88.9
0.
0.
0.
0
ST-9180
Body Tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
48
1
0
2
blue
0.
0.
0.
0.
1
0
8
0
76.2
25.3492
24.13
177.8
0
1
24.
6.35
0.
0.
1
0
Estes
1.40047
0.
Engine hook
123.825
1
123.825
0.
0.
0.
0.
0.
0
Engine hook
Standard size
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
49
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
200.025
0
0.
Semroc
0.
337.541
1/8 Aircraft Plywood
Centering ring
0.
0
0.
1.22183
1.5875
0.
0.
0.
0
CR-913
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
50
0
0
2
blue
0.
0.
0.
0.
1
0
8
0
149.225
38.1
25.3492
3.175
3
0
0
Semroc
0.
337.541
1/8 Aircraft Plywood
Centering ring
0.
0
73.025
1.22183
1.5875
0.
0.
0.
0
CR-913
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
51
0
0
2
blue
0.
0.
0.
0.
1
0
8
0
76.2
38.1
25.3492
3.175
3
0
0
Custom
0.
337.541
1/8 Aircraft Plywood
Lower fins
0.
0
0.
4.32133
48.3023
0.00717741
0.00717741
0.
0
0.
-2.61799
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
52
0
0
2
blue
11.7844
0.110919
26.3876
0.111023
1
0
8
0
76.2
1
76.2
39.22
60.33
65.6309
44.33
3.175
2
0
0
69.85
6.35
3.175
1
0.
0.
47.1342
30.4698
0.514698
0.
0.
59.79
39.2174
76.2,0|88.9,25.4|76.2,50.8|50.8,60.325|0,50.8|25.4,50.8|25.4,25.4|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
798.85
Afterburner front
0.
0
314.96
28.737
25.005
0.00465084
0.00465084
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
rgb(206,211,255)
white
1
53
0
0
0
blue
3.21248
0.176316
3.21248
0.176316
1
0
8
0
152.4
25.3746
40.386
44.45
0
0.
0.
1
12.7
0.
0.
0.
0
0.
119.59
75.1396
Semroc
0.
848.979
Spiral/Glassine
Afterburner
0.
0
359.41
0.759677
3.175
0.000805665
0.000805665
0.
0
LT-150300
Large Body Tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
54
1
0
0
blue
0.
0.
0.
0.
1
0
8
0
196.85
40.386
38.1
6.35
0
0
0.
0.5
0.
0.
0
0
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
0.594641
44.8252
0.00207306
0.00207306
0.
0
0.
-0.261799
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
55
0
0
2
blue
2.67331
0.179792
1.77897
0.184337
1
0
8
0
152.4
1
101.6
28.02
25.4
28.7554
23.31
1.5875
2
0
0
0.
0.
0.
1
0.
0.
22.9844
6.87341
0.275787
0.
0.
57.26
28.0209
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
0.594641
44.8252
0.00207306
0.00207306
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
56
0
0
2
blue
2.67331
0.179792
3.4367
0.184337
1
0
8
0
152.4
1
101.6
28.02
25.4
28.7554
23.31
1.5875
2
0
0
0.
0.
0.
1
0.
0.
22.9844
6.87341
0.275787
0.
0.
57.26
28.0209
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
0.594641
44.8252
0.00207306
0.00207306
0.
0
0.
0.261799
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
57
0
0
2
blue
2.67331
0.179792
4.86023
0.184337
1
0
8
0
152.4
1
101.6
28.02
25.4
28.7554
23.31
1.5875
2
0
0
0.
0.
0.
1
0.
0.
22.9844
6.87341
0.275787
0.
0.
57.26
28.0209
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
361.377
1/16 Aircraft Plywood
Cooling fin
0.
0
-50.8
1.06584
49.2963
0.00371577
0.00371577
0.
0
0.
-0.523599
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
58
0
0
2
blue
2.89663
0.17964
1.11857e-06
0.184492
1
0
8
0
152.4
1
101.6
29.69
25.4
28.753
22.48
1.5875
2
0
0
0.
0.
0.
1
0.
0.
33.6389
12.9448
0.292224
0.
0.
56.69
29.6872
101.6,0|47.625,25.4|0,6.35|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
798.85
afterburner rear
0.
0
365.76
32.8245
22.2473
0.00530446
0.00530446
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
rgb(206,211,255)
white
1
59
0
0
0
blue
-3.21248
0.226667
-3.21248
0.226667
1
0
8
0
203.2
40.386
25.3746
50.8
0
0.
0.
1
12.7
0.
0.
0.
0
0.
136.674
85.8738
Apogee
0.
1121.29
Paper
Launch lug
0.
0
25.4
1.11647
38.1
0.00374649
0.0019944
0.
0
13056
16.5608
3.14159
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
60
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
25.4
8.3312
7.2644
76.2
0
DynaStar Mid-Power Rockets
0.
0.
Polyethylene LDPE
Parachute
0.
0
0.
2.1445
67.7501
0.
0.
0.
0
29117
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
61
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
813.001
0.
8
8
0.024892
813.001
1
0.00032972
Carpet String (Apogee 29500)
0.75
926.75
142.743
454.689
11.3188
8.8025
1
37.3074
920.814
8
10.5163
0
2.51625
150.377
10.5163
0.925574
142.725
0.886982
116.687
21.3875
79.1846
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
0.
50.
15.
0.
0.
0
2
0.
0.89408
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
1.
1.
0.
0
0
3600.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
[F21W-8, F21W-8]
13.5006
0.
0.
0.13375
2.00125
10.5175
10
1
800.
0
Earth
Standard earth condistions.
2.282
79.1846
0.
7.19816
0.886983
-7.1433
0.
0,0,10.5163,0,0
-1,-1,-1,-1,-1
0,0,10.5163,0,0
32,32,80,32,32
1.
1
0.672522
0.0633663
0.0111091
0.00014234
0.0960174
72.7788
1.31709
{f36a4eb6-7809-4602-83d2-0917258bf322}
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
61
1
0.
0.
1
920.814
37.3074
-19.3655
10.5163
128
28,28,28
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
1
F21W
0.
Aerotech
6.35
0.
8
8.
0.
0.
1
F21W
0.
Aerotech
6.35
0.
48
8.
0.
0.
1174.5
160.639
720.01
12.4
8.82
1
47.2389
1167.85
8
11.58
0
3.58
230.751
11.58
0.968529
160.568
0.89408
103.219
55.1307
132.71
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
0.
50.
15.
0.
0.
0
2
0.
0.89408
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
1.
1.
0.
0
0
3600.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
[F23-8, F23-8]
13.124
0.
0.
0.14875
2.88125
11.5813
10
1
800.
0
Earth
Standard earth condistions.
1.672
132.71
0.
5.2779
0.63381
-5.23971
0.
0,0,11.58,0,0
-1,-1,-1,-1,-1
0,0,11.58,0,0
32,32,80,32,32
1.
1
0.695722
0.0636619
0.0108354
0.000252557
0.0960174
72.7788
1.30516
{45fae4a9-fccd-4403-b5e8-ed12c24b1888}
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
61
1
0.
0.
1
1167.85
47.2389
-43.4738
11.58
128
28,28,28
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
1
F23
0.
Ellis Mountain Rocket Works
6.35
0.
8
8.
0.
0.
1
F23
0.
Ellis Mountain Rocket Works
6.35
0.
48
8.
0.
0.
112.788
39.1943
85.7255
5.55875
3.9075
1
10.7682
106.95
5
6.65125
2
1.65125
27.0137
6.65125
1.52502
39.1584
0.723141
85.7255
0.0271153
9.15607
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
0.
50.
15.
0.
0.
0
2
0.
0.89408
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
1.
1.
0.
0
0
3600.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
[D12-5, D12-5]
11.0813
0.
0.
0.30375
1.62375
0.2825
10
1
800.
0
Earth
Standard earth condistions.
0.343
4.80387
0.
5.23289
0.723145
-5.18268
0.
0,0,6.65125,0,0
-1,-1,-1,-1,-1
0,0,6.65125,0,0
32,32,80,32,32
1.
1
0.629722
0.0549993
0.0104096
9.25384e-05
0.0960174
72.7788
1.6546
{6c132e90-abb6-4142-9210-6e1cb23242e1}
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0
0
0.
0.
0
0.
0.
0.
0.
-1
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
61
1
0.
0.
1
106.95
10.7682
-9.15607
6.65125
128
28,28,28
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
1
D12
0.
Estes
6.35
0.
8
5.
0.
0.
1
D12
0.
Estes
6.35
0.
48
5.
0.
0.