3
Aerotech Cheetah
1
0.75
0.78
0.8
0.95
0.95
1
292.
0.
0.
0.
0.
527.05
0.
0.
4
914.4
1
1
0
2
0
Stock Aerotech Cheetah--Weights and CG are set in over-ride based on measured values - Design entered by G.A. Dean
File from www.rocketreviews.com
4
196
1
0
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0,666.577,0,0
0,18.9147,0,0
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0
0
0.
10.
10.
10.
10.
9
1
0.
0.
0
0.
0.
0.
0.
-1
Custom
0.
1049.21
Polystyrene PS
Nose cone
0.
0
0.
33.5806
177.324
0.0235787
0.0235787
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.
0.10778
2.
0.10778
1
0
8
231.775
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.
37.8149
288.925
0.0876097
0.0876097
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
1
0
0
blue
0.
0.
0.
0.
1
0
8
48.26
46.99
577.85
1
0
0.
0.
0.
0.
0
Custom
0.
688.794
Cardboard
Body tube
0.
0
409.575
4.81887
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
8
0
0
blue
0.
0.
0.
0.
1
0
8
29.9974
29.0068
152.4
3
1
29.
12.7
0.
0.
1
Custom
0.
1199.78
Polycarbonate
Launch lug
0.
0
279.4
0.926499
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
530.225
0.926499
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
0.0254
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
19.05
64.6904
72.5081
0.00970966
0.0388386
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
2
blue
16.9147
0.73265
21.6952
0.73265
1
0
8
4
111.125
25.4
71.12
83.0376
85.725
3.175
0
1
2
0.
9.144
0.
1
0.879995
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
555.625
4.97224
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
46.99
29.9974
2.54
0
0
1
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
485.775
4.97224
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
46.99
29.9974
2.54
0
0
1
Custom
0.
1905.24
G10 fiberglass
Ring
0.
0
409.575
9.94447
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
46.99
29.9974
5.08
0
0
1
344.14
77.8485
73.0794
8.7225
6.
1
9.55348,0,0,0,0,0,0,0,0,0
339.29,0,0,0,0,0,0,0,0,0
7,0,0,0,0,0,0,0,0,0
9.72,0,0,0,0,0,0,0,0,0
1
2.7225
0.
9.72
1.52577
77.8485
0.
73.0794
0.
0.
0.
0.
1.2192
0
0.
0
0.
760.
1.5708
50.
15.
0.
0
2
0.
1.29642
1
0.
0.02
0
6
1.
1.
1
0.
0
3
300.
2000.
1
6.
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[E15-7 ]
12.2791
0.
0.
0.21
2.38
0.04
400.
0
earth
earth
1.20794
0.
0.
0.
0.
0,0,0
-1,-1,9.72
0,0,9.72
32,32,80
1.
5
0.3372
0.559854
0.0216254
8.46166e-05
9
1
0.
0.
1
339.29
9.55348
0.
9.72
7
1
E15
0.
A-WL
12.7
0.
3
7.
394.679
108.233
145.291
8.41
7.18875
1
1.92568
394.502
7
8.22125
0
1.22125
86.2912
8.22125
0.653459
108.233
0.100854
145.291
0.0047504
2.28029
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]
16.0696
0.
0.
0.1225
1.07375
0.04125
800.
0
Earth
Standard earth condistions.
4.921
2.28029
5.04489
0.100857
-5.04388
0,0,8.22125
-1,-1,8.22
0,0,8.22125
32,32,80
1.
1
0.3353
0.558655
0.0206092
7.55984e-05
9
1
0.
0.
1
394.502
1.92568
-0.0644263
8.22125
128
1
E30
0.
Aerotech
12.7
0.
3
7.
622.202
137.283
152.022
10.105
7.425
1
5.35447
621.213
7
9.68
0
2.68
112.061
9.68
0.679718
137.281
0.696116
152.022
0.699457
44.6773
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]
15.6835
0.
0.
0.1175
1.74875
0.01
800.
0
Earth
Standard earth condistions.
6.31
44.6773
5.59347
0.696121
-5.54999
0,0,9.68
-1,-1,9.68
0,0,9.68
32,32,80
1.
1
0.3666
0.5755
0.0192441
8.36217e-05
9
1
0.
0.
1
621.213
5.35447
-4.32026
9.68
128
1
F20EJ
0.
Aerotech
12.7
0.
3
7.
536.191
123.349
140.269
9.62125
7.4
1
5.13157
535.306
7
9.22
0
2.22125
114.944
9.22
0.768524
123.329
0.792003
140.269
2.21324
50.5432
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]
14.8348
0.
0.
0.135
1.7675
0.03
800.
0
Earth
Standard earth condistions.
6.41
50.5432
5.05748
0.370631
-5.04388
0,0,9.22
-1,-1,9.22
0,0,9.22
32,32,80
1.
1
0.3759
0.580188
0.0189141
8.5127e-05
9
1
0.
0.
1
535.306
5.13157
-11.777
9.22
128
1
F23FJ
0.
Aerotech
12.7
0.
3
7.
663.448
135.783
138.457
10.77
8.08
1
8.91823
659.334
9
11.69
2
2.69
125.751
11.69
0.683621
135.762
0.89408
138.457
0.389891
83.1055
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]
15.6067
0.
0.
0.135
1.89875
0.04
800.
0
Earth
Standard earth condistions.
6.972
83.1055
5.58007
0.779454
-5.52537
0,0,11.69
-1,-1,11.69
0,0,11.69
32,32,80
1.
1
0.3892
0.584628
0.0203987
0.000133872
9
1
0.
0.
1
659.334
8.91823
-15.5223
11.69
128
1
F25
0.
Aerotech
12.7
0.
3
9.
573.001
121.007
87.8356
10.4413
7.83125
1
11.137
566.429
9
11.61
2
2.61
112.644
11.61
1.10048
120.979
0.89408
87.8356
0.419328
70.6107
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]
12.3273
0.
0.
0.1675
2.18
0.04125
800.
0
Earth
Standard earth condistions.
6.023
70.6107
5.57482
0.786534
-5.51905
0,0,11.61
-1,-1,11.61
0,0,11.61
32,32,80
1.
1
0.3927
0.586169
0.0203386
0.000136223
9
1
0.
0.
1
566.429
11.137
-16.9346
11.61
128
1
F26FJ
0.
Aerotech
12.7
0.
3
9.
525.52
129.002
176.971
9.55
8.07875
1
0.901687
525.49
8
9.47
1
1.47125
105.159
9.47
0.546339
129.
0.388753
176.971
0.150674
14.5316
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]
17.4167
0.
0.
0.1075
1.1775
0.01
800.
0
Earth
Standard earth condistions.
5.714
14.5316
5.45098
0.0513394
-5.45074
0,0,9.47
-1,-1,9.47
0,0,9.47
32,32,80
1.
1
0.368
0.576221
0.0208373
0.000106703
9
1
0.
0.
1
525.49
0.901687
-4.65191
9.47
128
1
F42T
0.
Aerotech
12.7
0.
3
8.
683.456
180.097
216.541
10.1838
8.7525
1
2.40511
683.158
9
10.43
2
1.43125
143.854
10.43
0.457424
180.097
0.255697
216.541
0.0140322
9.83039
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]
19.5955
0.
0.
0.1
1.1325
0.01375
800.
0
Earth
Standard earth condistions.
7.731
9.83039
5.05036
0.255702
-5.04388
0,0,10.43
-1,-1,10.43
0,0,10.43
32,32,80
1.
1
0.3818
0.581279
0.0187508
9.11424e-05
9
1
0.
0.
1
683.158
2.40511
-0.280923
10.43
128
1
F50T
0.
Aerotech
12.7
0.
3
9.
773.525
159.387
122.663
10.4013
7.76125
1
19.7066
769.203
7
9.64
0
2.64
146.65
9.64
0.823927
159.385
0.847306
116.787
2.59638
78.833
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]
14.3405
0.
0.
0.13875
2.1525
9.64125
800.
0
Earth
Standard earth condistions.
7.382
78.833
5.65428
0.847309
-5.59043
0,0,9.64
-1,-1,9.64
0,0,9.64
32,32,80
1.
1
0.4184
0.592762
0.0198967
0.000199191
9
1
0.
0.
1
769.203
19.7066
-5.30083
9.64
128
1
G38FJ
0.
Aerotech
12.7
0.
3
7.
929.098
211.602
204.827
11.4925
9.1925
1
7.83506
925.927
10
12.3
2
2.3
191.752
12.3
0.504975
211.584
0.754417
204.827
0.80678
56.075
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]
18.4653
0.
0.
0.10875
1.77
0.025
800.
0
Earth
Standard earth condistions.
9.436
56.075
5.04427
0.0623378
-5.04388
0,0,12.3
-1,-1,12.3
0,0,12.3
32,32,80
1.
1
0.415
0.591519
0.0182548
0.000124166
9
1
0.
0.
1
925.927
7.83506
-14.458
12.3
128
1
G40W
0.
Aerotech
12.7
0.
3
10.
913.321
245.084
316.266
11.0763
9.665
1
3.2605
912.773
10
11.41
2
1.41125
188.595
11.41
0.323175
245.083
0.798642
316.266
0.0747572
79.4948
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]
22.9609
0.
0.
0.085
1.15375
0.01625
800.
0
Earth
Standard earth condistions.
9.307
79.4948
5.10672
0.798645
-5.04388
0,0,11.41
-1,-1,11.41
0,0,11.41
32,32,80
1.
1
0.4081
0.588934
0.0183269
0.000118069
9
1
0.
0.
1
912.773
3.2605
-1.04568
11.41
128
1
G80T
0.
Aerotech
12.7
0.
3
10.