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Vidar
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A build from various junk laying around. Another Simulation By Bruce S. Levison.
Craig A. Swinson
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0
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-1
28,28,28
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
0,0,0
Apogee
74.4997
1049.21
Polystyrene PS
Nose cone
65.405
1
0.
94.9722
188.986
0.0320124
0.0320124
0.
0
Apogee
PNC-80A
0.
0.
file=(C:/Documents and Settings/Admin/Desktop/nose.JPG)|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=(0)
0.
0.
1.
0.
1.
blue
rgb(85,170,0)
white
1
1
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0
0
rgb(85,170,0)
2.
0.105956
2.
0.105956
0
0
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228.6
66.04
0
1
1
69.85
1.88722
0.
66.548
0.
0.
0.
Apogee
0.
1121.29
Paper
Body tube
0.
0
0.
10.4859
177.8
0.0737766
0.0737766
0.
0
Apogee
BT-80
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(105,138,40)
white
0
3
9
0
0
rgb(170,170,0)
0.
0.
0.
0.
0
0
8
66.04
65.786
355.6
0
0
24.
0.
0.
0.
0
Apogee
0.
0.00440737
1.3 oz. Ripstop Nylon (SkyAngle)
Parachute
0.
0
130.175
6.63495
38.1
0.
0.
0.
1
29115
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
243
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0
0
rgb(255,128,0)
0.
0.
0.
0.
1
0
8
457.2
0.
6
6
0.0254
609.6
1
0.000178
30 Lb. kevlar
0.75
Custom
0.
0.00112861
300lb Kevlar (Apogee 29506)
Shock Cord
219.075
0
219.075
1.032
0.
0.
0.
0.
2
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
193
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0
0
rgb(227,228,0)
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0.
0.
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0
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1
914.4
Custom
0.
128.148
Balsa
Strakes (Fin set)
0.
0
114.3
1.0826
69.7284
0.00235887
0.0070766
0.
0
0.
-1.0472
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(0,0,0)
white
1
117
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0
0
rgb(0,0,0)
0.221359
0.381503
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1
0
8
3
139.7
107.95
9.525
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15.621
2.3876
0
0
0
0.
0.
0.
0
1.0232
0.
37.579
0.264064
0.772727
0.
0.
Apogee
0.
1121.29
Paper
Forward Centering Ring
0.
0
260.35
10.3825
1.5875
0.
0.
0.
0
13035
CR 24-29
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(0,128,0)
white
1
6
8
0
0
rgb(0,128,0)
0.
0.
0.
0.
1
0
8
65.786
24.7904
3.175
0
0
1
Apogee
0.
1121.29
Paper
Engine Mount tube
0.
0
247.65
3.07134
53.975
0.
0.
0.
0
10099
24 mm
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(204,204,204)
white
1
5
9
0
0
rgb(128,128,0)
0.
0.
0.
0.
1
0
8
24.7904
24.13
107.95
0
1
24.
0.
0.
0.
1
Apogee
0.
1121.29
Paper
Engine Block Ring
0.
0
101.6
1.28043
3.175
0.
0.
0.
0
13031
CR 18-24 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
rgb(0,128,0)
white
1
8
8
0
2
rgb(216,0,0)
0.
0.
0.
0.
1
0
8
24.13
18.796
6.35
0
2
1
Apogee
0.
1121.29
Paper
Aft Centering Ring
0.
0
342.9
10.3825
1.5875
0.
0.
0.
0
13035
CR 24-29
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(204,204,204)
white
1
7
8
0
0
rgb(0,128,0)
0.
0.
0.
0.
1
0
8
65.786
24.7904
3.175
0
0
1
LOC
0.
1121.29
Paper
Launch lug
0.
0
257.175
0.514119
38.1
0.00289425
0.00152012
0.
0
LOC LL25
LL-25
36.195
1.93077
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(0,0,0)
white
1
10
8
0
0
rgb(76,76,76)
0.
0.
0.
0.
1
0
8
6.35
5.715
76.2
0
Custom
0.
128.148
Balsa
Aft Fin set
0.
0
266.7
2.81291
32.4184
0.00612902
0.0183871
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(0,0,0)
white
1
118
0
0
0
rgb(0,0,0)
4.14045
0.511509
6.81855
0.511509
1
0
8
3
88.9
31.75
50.8
58.2853
0.
2.3876
0
0
1
0.
0.
0.
0
0.
0.
54.4095
3.93669
0.357143
0.
0.
399.243
97.4837
92.0452
9.105
6.0125
1
21.492
378.818
4
7.09
2
3.0925
88.9525
7.09
1.17603
96.9777
3.53163
92.0452
2.61745
146.534
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
1.571
0.
50.
15.
0.
0.
0
3
1.34112
3.53162
4
0.09
0.02
0
6
1.
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.
[E9-4]
11.6848
0.
0.
0.2725
3.0275
0.27
10
1
400.
0
Earth
Standard earth condistions.
20.363
146.534
0.
5.66902
2.71778
-4.97509
0.
0,0,7.09,0,0
-1,-1,-1,-1,-1
0,0,9.105,0,0
32,32,80,32,32
0.25
1
0.193074
0.309994
0.0115802
8.36738e-05
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-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
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0.
0
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-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
243
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1
399.243
4.85348
-45.982
9.105
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
E9
0.
Estes
0.
0.
5
4.
0.
0.
249.151
79.1675
173.938
6.94875
5.2975
1
3.57057
248.685
5
6.65125
0
1.65125
59.375
6.65125
0.868815
79.1412
2.61023
173.2
16.0094
134.489
0.
0.
0
1524.
0
0.
0
0.0872665
0.
0.
759.813
1.571
0.
50.
15.
0.
0.
0
99
2.2352
2.2352
1
0.
0.02
0
6
1.
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]
19.7688
0.
0.
0.28
1.615
0.28125
10
1
800.
0
Earth
Standard earth condistions.
0.453
134.489
0.
5.25431
2.2352
-4.75517
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
0.164779
0.310149
0.0093664
8.23216e-05
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-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
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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
243
1
0.
0.
1
248.685
3.57057
17.0164
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
0.
0.
5
5.
0.
0.
105.52
47.9922
130.622
4.76875
3.9575
1
9.40835
100.497
5
5.81125
2
0.81125
26.5762
5.81125
0.952854
47.9555
2.31766
130.051
12.1966
60.3975
0.
0.
0
1524.
0
0.
0
0.0872665
0.
0.
759.813
1.571
0.
50.
15.
0.
0.
0
99
2.2352
2.2352
1
0.
0.02
0
6
1.
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.
[C11-5]
17.8879
0.
0.
0.29
0.78375
0.2975
10
1
800.
0
Earth
Standard earth condistions.
0.219
60.3975
0.
5.2812
2.2352
-4.78487
0.
0,0,5.81125,0,0
-1,-1,-1,-1,-1
0,0,5.81125,0,0
32,32,80,32,32
1.
1
0.157479
0.299068
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-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
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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
243
1
0.
0.
1
100.497
9.40835
13.9836
5.81125
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
C11
0.
Estes
0.
0.
5
5.
0.
0.