3
SHR 1/48th Scale Saturn V
1
0.9
0.78
0.8
0.95
0.95
1
3855.54
0.
0.
0.
0.
1087.12
0.
0.
4
1220.42
1
1
0
2
0
Note: The reference diameter is set to use the maximum frontal area. But even so, RockSim will always tell you if the rocket will be stable by looking at the 2D flight profile.
Tim Van Milligan. Visit my web site at: www.ApogeeRockets.com
Dimensions may not be 100% accurate. Please check them yourself!
4
215
1
0
CSV1|1|989.013,-1.13687e-13,0|1961.48,-191.384,-530.836|-0.0478496,0.908474,-0.415193|36.2944,3629.44|30|2|1124.33|22.7903|0|0|0|0
0,1280.79,0,0
0,25.3717,0,0
0,1353.45,0,0
0,28.3199,0,0
0
1
0
1
0.
0.
0
0
0
0
3
0
0
1
0.
9.99998
10.0076
10.0076
10.0076
213
1
0.
0.
0
0.
0.
0.
0.
-1
215
1
0.
0.
0
0.
0.
0.
0.
-1
Custom
0.
1185.37
Acrylic (Cast)
Nose cone
0.
0
0.
45.6902
69.6162
0.0115385
0.0115385
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(255,255,255)
white
1
1
0
0
0
rgb(0,0,0)
2.
0.0465201
2.
0.0465201
1
0
8
69.85
88.9
0
0
0
12.7
0.762
0.
54.7624
0.
0.
0.
Custom
92.
0.
92g clay nose mass
0.
1
28.575
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
60
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
0.
uline
0.
1121.29
Paper
Service Module Body tube (Front Part)
0.
0
0.
37.3413
47.625
0.0266021
0.0266021
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(179,179,179)
white
1
2
1
0
0
rgb(51,51,51)
0.
0.
0.
0.
1
0
8
88.9
86.36
95.25
0
0
0.
0.
0.
0.
0
Custom
0.
1121.29
Paper
Transition (LEM area)
0.
0
0.
23.5256
96.6385
0.0636547
0.0636547
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(255,255,255)
white
1
3
1
0
0
rgb(128,0,64)
2.5
0.26162
2.5
0.26162
1
0
8
88.9
133.35
180.975
0
0.
0.
1
0.3302
0.
0.
0.
0
0.
542.925
361.95
Uline
0.
1121.29
Paper
3rd Stage tube (front portion)
0.
0
0.
397.54
136.525
0.114389
0.114389
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(255,255,255)
white
1
5
1
0
0
rgb(0,0,128)
0.
0.
0.
0.
1
0
8
133.35
127.
273.05
0
0
0.
0.
0.
0.
0
Dynastar
0.
0.006685
Rip stop nylon
Parachute
0.
0
412.75
109.788
127.
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
rgb(255,128,0)
white
1
215
0
0
0
rgb(255,128,0)
0.
0.
0.
0.
1
0
8
1524.
0.
8
8
0.
0.
1
0.00102
1/16 In. braided nylon
0.75
Custom
0.
1049.21
Polystyrene PS
2nd to 3rd stage Transition
0.
0
0.
41.4432
75.04
0.077899
0.077899
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(230,230,230)
white
1
80
1
0
0
rgb(0,64,128)
6.61224
0.694149
6.61224
0.694149
1
0
8
133.35
209.55
139.7
0
0.
0.
1
0.508
0.
0.
0.
0
0.
384.175
244.475
Uline
0.
1121.29
Paper
Main Body Tube
0.
0
0.
2814.13
609.6
0.802625
0.802625
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(255,255,255)
white
1
82
1
0
0
rgb(0,0,0)
0.
0.
0.
0.
1
0
8
209.55
203.2
1219.2
0
0
0.
0.
0.
0.
0
Custom
0.
344.269
1/4 Aircraft Plywood
Forward motor tube centering disk
0.
0
381.
65.4129
3.175
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
rgb(0,128,64)
white
1
87
0
0
0
rgb(0,128,0)
0.
0.
0.
0.
1
0
8
203.2
56.5
6.35
3
0
1
Custom
0.
344.269
1/4 Aircraft Plywood
Rear motor tube centering disk
0.
0
1168.4
65.4129
3.175
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
rgb(0,128,64)
white
1
91
0
0
0
rgb(0,128,0)
0.
0.
0.
0.
1
0
8
203.2
56.5
6.35
0
0
1
Custom
0.
1049.21
Polystyrene PS
Custom Fin set
0.
0
0.
154.825
112.186
0.0154511
0.0618046
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(255,255,255)
white
1
92
0
0
2
rgb(128,0,128)
14.2595
1.90461
17.2076
1.91732
1
0
8
4
159.85
73.97
109.88
138.584
127.39
4.7752
2
0
1
0.
0.
0.
0
0.
70.53
73.9686
159.852,0|159.335,37.2236|148.169,37.2352|148.245,109.875|116.134,109.875|66.3213,17.9285|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.
958.705
Kraft phenolic
motor mount 1
0.
0
330.2
179.635
431.8
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
211
0
0
0
blue
0.
0.
0.
0.
1
0
8
56.5
54.
863.6
0
1
54.
12.7
0.
0.
1
DYNASTAR
0.
0.006685
Rip stop nylon
Parachute
0.
0
330.2
102.591
122.767
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
rgb(255,128,0)
white
1
213
0
0
0
rgb(255,128,0)
0.
0.
0.
0.
1
0
8
1473.2
0.
8
8
0.
0.
2
0.00102
1/16 In. braided nylon
0.75
89.1542
36.0365
44.3851
4.76125
3.35
1
6.32391
87.0943
4
5.41125
2
1.41125
17.5213
5.41125
2.35158
36.0307
0.58427
44.3851
0.0282533
4.08757
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
2
0.
0.89407
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-4, G80T-4]
8.461
0.
0.
0.2225
1.19375
0.01625
800.
0
Earth
Standard earth condistions.
0.406
4.08757
7.22681
0.531874
-7.20721
0,0,5.41125
-1,-1,5.41
0,0,5.41125
32,32,80
1.
1
4.08774
1.13346
1.61961
0.0336733
214
1
0.
0.
1
87.0943
6.32391
-2.67232
5.41125
128
213
1
0.
0.
0
0.
0.
0.
0.
-1
1
G80T
0.
Aerotech
12.7
0.
211
4.
1
G80T
0.
Aerotech
12.7
0.
212
4.
89.1036
36.0315
44.3851
4.76
3.34875
1
6.37227
87.034
4
5.41125
2
1.41125
21.8387
5.41125
2.35153
36.0184
0.892936
44.3851
0.0432429
10.7462
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
2
0.
0.89407
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-4, G80T-4]
8.461
0.
0.
0.2225
1.19375
0.01625
800.
0
Earth
Standard earth condistions.
0.453
10.7462
5.34492
0.881731
-5.27169
0,0,5.41125
-1,-1,5.41
0,0,5.41125
32,32,80
1.
1
4.08774
1.13346
1.52419
0.0337494
213
1
0.
0.
1
87.034
6.37227
-3.84677
5.41125
128
215
1
0.
0.
0
0.
0.
0.
0.
-1
1
G80T
0.
Aerotech
12.7
0.
211
4.
1
G80T
0.
Aerotech
12.7
0.
212
4.
89.2049
36.0416
44.3851
4.76375
3.3525
1
6.27681
87.1563
4
5.41125
2
1.41125
21.8625
5.41125
2.35162
36.0416
0.0145673
44.3851
0.00133378
0.138784
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
2
0.
0.89407
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-4, G80T-4]
8.46101
0.
0.
0.2225
1.19375
0.01625
800.
0
Earth
Standard earth condistions.
0.313
-0.0199028
5.27169
0.00186956
-5.27169
0,0,5.41125
-1,-1,5.41
0,0,5.41125
32,32,80
1.
1
4.08774
1.13346
1.53627
0.0337515
213
1
0.
0.
1
87.1563
6.27681
-0.138784
5.41125
128
215
1
0.
0.
0
0.
0.
0.
0.
-1
1
G80T
0.
Aerotech
12.7
0.
211
4.
1
G80T
0.
Aerotech
12.7
0.
212
4.
89.2033
36.0415
44.3851
4.76375
3.3525
1
6.27905
87.1543
4
5.41125
2
1.41125
18.35
5.41125
2.35162
36.0412
0.0835352
44.3851
0.00622903
0.643929
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
2
0.
0.89407
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-4, G80T-4]
8.46101
0.
0.
0.2225
1.19375
0.01625
800.
0
Earth
Standard earth condistions.
0.281
0.232539
6.74197
0.0530025
-6.74176
0,0,5.41125
-1,-1,5.41
0,0,5.41125
32,32,80
1.
1
4.08774
1.13346
1.53627
0.0337515
213
1
0.
0.
1
87.1543
6.27905
-0.643929
5.41125
128
215
1
0.
0.
0
0.
0.
0.
0.
-1
1
G80T
0.
Aerotech
12.7
0.
211
4.
1
G80T
0.
Aerotech
12.7
0.
212
4.
454.495
74.9713
22.5427
12.0063
3.745
0
4
8.26125
22.6025
0.
5.23927
67.0907
0.
22.5423
0.0635798
8.03404
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
2
0.
0.89407
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.
[I65W-None]
5.28389
0.
0.
0.45
22.6012
1.72375
800.
0
Earth
Standard earth condistions.
0.5
-8.03404
74.9758
-0.242292
-74.9754
0,0,0
-1,-1,1.6e+308
0,0,0
32,32,32
1.
1
4.63164
1.21457
1.63611
0.036504
213
1
0.
0.
0
0.
0.
0.
0.
-1
215
1
0.
0.
0
0.
0.
0.
0.
-1
1
I65W
0.
Aerotech
12.7
0.
211
-2.