3
Aerotech Mustang
1
0.75
0.78
0.8
0.95
0.95
1
311.845
0.
0.
0.
0.
0.
0.
0.
4
914.4
0
1
0
2
0
Stock Aerotech Mustang--Weights are not accurate--11oz has been specified as the weight. Design entered by Andy Tate
Original RockSim file from www.RocketReviews.com
4
15
1
0
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0,771.665,0,0
0,32.5441,0,0
0,778.798,0,0
0,39.45,0,0
0
1
0
1
0.
0.
0
0
0
0
0
0
0
0
0.
10.
9.99998
9.99998
9.99998
9
1
0.
0.
0
0.
0.
0.
0.
-1
Custom
0.
1049.21
Polystyrene PS
Nose cone
0.
0
0.
42.8313
233.577
0.0325223
0.0325223
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
1
0
0
0
blue
2.
0.149372
2.
0.149372
1
0
8
320.675
48.26
1
1
1
50.8
1.016
0.
45.72
0.
0.
0.
Custom
0.
688.794
Cardboard
Body tube
0.
0
0.
75.4414
292.1
0.0885725
0.0885725
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
2
0
0
0
blue
0.
0.
0.
0.
1
0
8
48.26
45.72
584.2
1
0
0.
12.7
0.
0.
0
Custom
0.
688.794
Cardboard
Body tube
0.
0
409.575
4.81594
76.2
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
3
0
0
0
blue
0.
0.
0.
0.
1
0
8
29.997
29.007
152.4
3
1
29.
12.7
0.
0.
1
Custom
0.
1199.78
Polycarbonate
Launch lug
0.
0
279.4
0.926497
12.7
0.0012465
0.00070939
0.
0
28.575
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
7
0
0
0
blue
0.
0.
0.
0.
1
0
8
8.89
6.35
25.4
1
Custom
0.
1199.78
Polycarbonate
Launch lug
0.
0
536.575
0.926497
12.7
0.0012465
0.00070939
0.
0
28.575
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
8
0
0
0
blue
0.
0.
0.
0.
1
0
8
8.89
6.35
25.4
1
Custom
0.
0.006685
Rip stop nylon
Parachute
0.
0
165.1
24.5085
46.5667
0.
0.
0.
1
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
9
0
0
0
blue
0.
0.
0.
0.
1
0
8
558.8
0.
0
6
0.025
558.8
1
0.00242
5/64 In. round elastic
0.75
Custom
0.
0.00402
1/4 In. flat elastic
Mass object
0.
0
257.175
7.35178
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
10
0
0
0
blue
0.
0.
0.
0.
1
0
8
1
1828.8
Custom
28.35
0.
Inside Fins
0.
1
485.775
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
11
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
Custom
2.835
0.
Motor Hook
0.
1
565.15
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
12
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
Custom
28.35
0.
Eye Screw and Baffle
0.
1
409.575
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
13
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
Custom
56.699
0.
Cooling Mesh
0.
1
444.5
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
14
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
Custom
0.
1049.21
Polystyrene PS
Fin set
0.
0
412.75
130.67
107.694
0.0196129
0.0784515
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
15
0
0
0
blue
30.5441
0.812412
37.45
0.812412
1
0
8
4
165.1
38.1
96.52
115.547
127.022
3.175
0
1
2
0.
0.
0.
1
0.92
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
555.625
4.52483
1.27
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
4
0
0
0
blue
0.
0.
0.
0.
1
0
8
45.72
29.997
2.54
0
0
1
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
485.775
4.52483
1.27
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
5
0
0
0
blue
0.
0.
0.
0.
1
0
8
45.72
29.997
2.54
0
0
1
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
409.575
9.04966
2.54
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
6
0
0
0
blue
0.
0.
0.
0.
1
0
8
45.72
29.997
5.08
0
0
1
243.737
60.4918
70.7823
7.705
5.065
1
17.6029
226.022
7
9.64
2
2.64
46.3125
9.64
1.98445
60.4827
0.275779
70.7823
0.102064
7.43215
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[E15-7]
9.39985
0.
0.
0.2025
2.31125
9.64125
800.
0
Earth
Standard earth condistions.
6.93
0.0755238
6.06395
0.139109
-6.06236
0,0,9.64
-1,-1,9.64
0,0,9.64
32,32,80
1.
1
0.471905
0.710946
0.0272955
0.000163002
9
1
0.
0.
1
226.022
17.6029
-7.43215
9.64
128
1
E15
0.
Aerotech
12.7
0.
3
7.
258.608
75.3686
99.644
7.26
6.03875
1
9.28245
254.114
7
8.22125
2
1.22125
40.0612
8.22125
0.958783
75.3653
0.642288
99.644
0.0831139
14.3607
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[E30-7]
13.2517
0.
0.
0.14625
1.08375
0.04125
800.
0
Earth
Standard earth condistions.
9.233
14.3607
7.9607
0.642293
-7.93475
0,0,8.22125
-1,-1,8.22
0,0,8.22125
32,32,80
1.
1
0.465105
0.708761
0.0274959
0.000162895
9
1
0.
0.
1
254.114
9.28245
-3.96416
8.22125
128
1
E30
0.
Aerotech
12.7
0.
3
7.
450.454
99.1661
105.523
9.37875
6.69875
1
2.95163
450.007
7
9.68
2
2.68
68.3162
9.68
0.985164
99.1658
0.315353
105.523
0.0302645
10.1826
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F20EJ-7]
12.9777
0.
0.
0.14125
1.8275
0.01
800.
0
Earth
Standard earth condistions.
9.184
10.1826
7.71979
0.315358
-7.71335
0,0,9.68
-1,-1,9.68
0,0,9.68
32,32,80
1.
1
0.496405
0.717343
0.0268897
0.000170918
9
1
0.
0.
1
450.007
2.95163
-1.60781
9.68
128
1
F20EJ
0.
Aerotech
12.7
0.
3
7.
374.198
88.0203
97.4027
8.7475
6.52625
1
4.77426
373.102
7
9.22
2
2.22125
70.3062
9.22
1.12889
88.001
0.698437
97.4027
0.238649
23.794
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F23FJ-7]
12.1949
0.
0.
0.16
1.825
0.03
800.
0
Earth
Standard earth condistions.
9.384
23.794
6.07837
0.440955
-6.06236
0,0,9.22
-1,-1,9.22
0,0,9.22
32,32,80
1.
1
0.505705
0.719853
0.0267373
0.000172424
9
1
0.
0.
1
373.102
4.77426
-11.2486
9.22
128
1
F23FJ
0.
Aerotech
12.7
0.
3
7.
537.082
113.591
115.446
10.0088
7.31875
1
15.5517
523.632
9
11.69
2
2.69
77.3187
11.69
0.831127
113.575
0.595127
115.446
0.280636
15.9031
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F25-9]
14.2138
0.
0.
0.14625
1.9125
0.04
800.
0
Earth
Standard earth condistions.
10.385
15.9031
7.94373
0.306995
-7.9378
0,0,11.69
-1,-1,11.69
0,0,11.69
32,32,80
1.
1
0.519005
0.721882
0.0266113
0.000181933
9
1
0.
0.
1
523.632
15.5517
-13.7093
11.69
128
1
F25
0.
Aerotech
12.7
0.
3
9.
455.528
100.32
72.6576
9.6425
7.0325
1
17.8236
437.263
9
11.61
2
2.61
82.575
11.61
1.33538
100.319
0.100325
72.6576
0.0618369
3.32194
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F26FJ-9]
11.1675
0.
0.
0.1825
2.185
0.04125
800.
0
Earth
Standard earth condistions.
11.597
-1.00098
6.06236
0.000156646
-6.06236
0,0,11.61
-1,-1,11.61
0,0,11.61
32,32,80
1.
1
0.522505
0.722716
0.0266147
0.000184822
9
1
0.
0.
1
437.263
17.8236
-3.32194
11.61
128
1
F26FJ
0.
Aerotech
12.7
0.
3
9.
411.03
104.863
143.335
8.74
7.26875
1
7.08923
408.429
8
9.47
2
1.47125
65.9312
9.47
0.670909
104.862
0.237101
143.335
0.0819759
4.53819
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F42T-8]
15.7581
0.
0.
0.12
1.1825
0.01
800.
0
Earth
Standard earth condistions.
9.544
4.53819
7.09557
0.0584994
-7.09533
0,0,9.47
-1,-1,9.47
0,0,9.47
32,32,80
1.
1
0.497805
0.717726
0.0268001
0.000169413
9
1
0.
0.
1
408.429
7.08923
-3.34319
9.47
128
1
F42T
0.
Aerotech
12.7
0.
3
8.
519.733
130.338
151.996
9.5375
8.10625
1
8.65598
515.856
9
10.43
2
1.43125
75.1612
10.43
0.639493
130.324
0.858045
151.996
0.343814
39.6133
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[F50T-9]
16.2583
0.
0.
0.1175
1.1525
0.01375
800.
0
Earth
Standard earth condistions.
11.146
39.6133
7.92596
0.668868
-7.89769
0,0,10.43
-1,-1,10.43
0,0,10.43
32,32,80
1.
1
0.511605
0.720082
0.0266699
0.000178439
9
1
0.
0.
1
515.856
8.65598
-10.5526
10.43
128
1
F50T
0.
Aerotech
12.7
0.
3
9.
651.266
136.555
100.183
10.3425
7.7025
1
12.282
648.121
7
9.64
0
2.64
92.2925
9.64
0.956066
136.555
0.473343
100.183
0.605163
22.0507
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[G38FJ-7]
13.2091
0.
0.
0.14875
2.1575
0.025
800.
0
Earth
Standard earth condistions.
12.568
22.0507
7.84706
0.473348
-7.83277
0,0,9.64
-1,-1,9.64
0,0,9.64
32,32,80
1.
1
0.548205
0.725514
0.026499
0.00021756
9
1
0.
0.
1
648.121
12.282
-2.26064
9.64
128
1
G38FJ
0.
Aerotech
12.7
0.
3
7.
751.181
160.156
146.194
11.155
8.855
1
10.9437
744.819
10
12.3
2
2.3
132.797
12.3
0.69268
160.156
0.230755
146.194
0.0103426
8.1983
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[G40W-10]
15.5829
0.
0.
0.1275
1.85875
0.025
800.
0
Earth
Standard earth condistions.
20.88
8.1983
6.06675
0.23076
-6.06236
0,0,12.3
-1,-1,12.3
0,0,12.3
32,32,80
1.
1
0.544805
0.724841
0.0264752
0.000211462
9
1
0.
0.
1
744.819
10.9437
-0.343556
12.3
128
1
G40W
0.
Aerotech
12.7
0.
3
10.
749.258
182.416
226.081
10.7938
9.3825
1
6.03608
747.404
10
11.41
2
1.41125
132.535
11.41
0.450328
182.406
0.729744
226.081
0.464365
48.2246
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
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
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[G80T-10]
19.434
0.
0.
0.1
1.18625
0.01625
800.
0
Earth
Standard earth condistions.
21.511
48.2246
6.06644
0.222359
-6.06236
0,0,11.41
-1,-1,11.41
0,0,11.41
32,32,80
1.
1
0.537905
0.72345
0.0265055
0.000205365
9
1
0.
0.
1
747.404
6.03608
-9.94079
11.41
128
1
G80T
0.
Aerotech
12.7
0.
3
10.