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RockSim File opened 10/08/12.
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Polystyrene PS
Body Tube #11
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Polystyrene PS
Transition #12
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1049.21
Polystyrene PS
Body Tube #13
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1/4 Aircraft Plywood
Aft Bottom Centering Ring
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Custom
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Aircraft plywood (LOC)
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Paper
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Motor mount tube
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12.7
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Custom
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344.269
1/4 Aircraft Plywood
Fin set-1
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26.8638
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Custom
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Fake Fin Pod
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337.541
1/8 Aircraft Plywood
Fin set
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0.014101
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Custom
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1/4 Aircraft Plywood
Fin set-2
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26.8638
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Custom
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Fake Fin Pod
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337.541
1/8 Aircraft Plywood
Fin set
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37.5513
0.014101
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1/4 Aircraft Plywood
Fin set-3
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Custom
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Fake Fin Pod
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93.5639
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337.541
1/8 Aircraft Plywood
Fin set
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0.930898
37.5513
0.014101
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344.269
1/4 Aircraft Plywood
Fin set-4
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1.10734
26.8638
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Custom
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Fake Fin Pod
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93.5639
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Custom
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337.541
1/8 Aircraft Plywood
Fin set
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0.930898
37.5513
0.014101
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344.269
1/4 Aircraft Plywood
Fin set-5
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26.8638
0.00502728
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Custom
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Fake Fin Pod
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93.5639
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Custom
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337.541
1/8 Aircraft Plywood
Fin set
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0.930898
37.5513
0.014101
0.014101
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66.9079
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Custom
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344.269
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Fin set-6
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1.10734
26.8638
0.00502728
0.00502728
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white
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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)
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759.813
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0.89408
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0.01
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2000.
1
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[C11-3]
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0.51875
0.77625
0.2975
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800.
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Earth
Standard earth condistions.
0.25
0.020744
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5.5245
0.00619757
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0,0,3.81,0,0
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Estes
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98.097
38.5027
89.5796
4.99
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3.79386
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0.0265382
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759.813
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0.89408
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0.01
0.02
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0.1
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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
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0.99
2000.
1500.
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0.98
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0
0.08
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1
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1
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1.
1.
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0
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3600.
0.
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0.
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0.
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0.
0.
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0.
0.
0.
0.
[D12-3]
17.7664
0.
0.
0.48125
1.615
0.2825
10
1
800.
0
Earth
Standard earth condistions.
0.375
-0.000132295
0.
5.95432
0.00704538
-5.95432
0.
0,0,4.65,0,0
-1,-1,-1,-1,-1
0,0,4.65,0,0
32,32,80,32,32
1.
1
301.926
104.606
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0.000140293
279.212
134.496
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-1
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1
97.497
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D12
0.
Estes
0.50038
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16
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177.168
75.2662
293.48
5.6225
5.2925
1
24.4419
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759.813
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2000.
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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
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0.99
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1500.
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0.98
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0.08
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[E75-VM-8]
43.664
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0.17625
0.325
0.0125
10
1
800.
0
Earth
Standard earth condistions.
0.577
1.66954
0.
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0.0588291
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0,0,8.33,0,0
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32,32,80,32,32
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1
311.326
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134.496
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-1
0,0,0
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53
1
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1
142.93
24.4419
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28,28,28
0,0,0
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0,0,0
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E75-VM
0.
Cesaroni Technology Inc.
0.50038
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16
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421.399
137.967
186.885
8.08
6.78125
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11.6998
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0.577565
137.947
0.87599
186.885
0.852024
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759.813
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0.89408
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0.01
0.02
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0.1
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2000.
1
5.99999
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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
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0.99
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1500.
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0.08
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3600.
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[60-F50-SK-13A-8]
34.8236
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0.21625
1.06
0.0225
10
1
800.
0
Earth
Standard earth condistions.
1.092
45.7657
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0.875991
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0.
0,0,9.29875,0,0
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32,32,80,32,32
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1
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279.212
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414.251
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60-F50-SK-13A
0.
CTI
0.50038
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16
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420.281
137.971
186.885
7.85375
6.555
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418.506
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7.29875
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0.577565
137.971
0.258685
186.885
0.0787159
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3657.6
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0
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0.
0.
759.813
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50.
15.
0.
0.
0
2
0.
0.89408
2
0.01
0.02
0
5
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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
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1.
1.
0.
0
0
3600.
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0.
0.
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0.
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0.
0.
0.
0.
[60-F50-SK-13A-6]
34.8236
0.
0.
0.21625
1.06
0.0225
10
1
800.
0
Earth
Standard earth condistions.
0.952
9.31036
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5.83835
0.25869
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0.
0,0,7.29875,0,0
-1,-1,-1,-1,-1
0,0,7.29875,0,0
32,32,80,32,32
1.
1
353.226
121.832
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0.000233732
279.212
134.496
5.16339
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0,0,0
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-1
0,0,0
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53
1
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418.506
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28,28,28
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0,0,0
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60-F50-SK-13A
0.
CTI
0.50038
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16
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512.444
157.817
227.933
8.63375
7.05625
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0.966132
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157.801
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20.7511
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759.813
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0.89408
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0.01
0.02
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0.1
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3
300.
2000.
1
5.99999
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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
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0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
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1
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1.
1.
0.
0
0
3600.
0.
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[75-F51-CL-12A-7]
37.8383
0.
0.
0.2
1.2975
0.03125
10
1
800.
0
Earth
Standard earth condistions.
0.999
20.7511
0.
5.86123
0.168686
-5.8588
0.
0,0,8.5775,0,0
-1,-1,-1,-1,-1
0,0,8.5775,0,0
32,32,80,32,32
1.
1
354.326
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279.212
134.496
5.1504
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0,0,0
0,0,0
0,0,0
0,0,0
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0.
0
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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
53
1
0.
0.
1
512.43
0.966132
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8.5775
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
75-F51-CL-12A
0.
CTI
0.50038
0.
16
7.
0.
0.