3
BARCLONE Antares
1
0.75
0.78
0.8
0.95
0.95
1
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1
914.4
0
1
0
2
0
Craig McGraw -- BARCLONE Rocketry
12-10-2005 -- Modified the tip pods with tubes; made minor adjustments to the fin shapes.
4
100
1
0
CSV1|1|301.527,-4.26326e-14,0|302.034,283.673,558.344|-0.000227559,0.891534,-0.452953|345.721,980.942|30|2|626.273|0.0105106|0|0|0|0
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-1
BMS
4.53592
128.148
Balsa
Nose cone
61.595
1
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2.66096
84.1679
0.00577132
0.00577132
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BNC-50Y
BNC-50Y
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24.13
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Semroc
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Screw Eye
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SE-10
Screw Eye
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BT-50
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LL-1/8
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Body tube
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EST 30386
BT-55J
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EST 30326
BT-20J
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18.034
69.85
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1
18.
6.35
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1
BMS
0.
724.996
Aircraft plywood (Birch)
Ring
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3.175
0.587968
1.5875
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CR-520
CR-520
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18.034
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3.175
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BMS
0.
724.996
Aircraft plywood (Birch)
Ring
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63.5
0.420831
1.5875
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CR-2050-W
CR-2050-W
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24.13
18.6944
3.175
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BMS
0.
724.996
Aircraft plywood (Birch)
Ring
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19.05
0.420831
1.5875
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CR-2050-W
CR-2050-W
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24.13
18.6944
3.175
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1
Custom
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128.148
Balsa
Custom Fin set
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0
0.
11.3125
59.3629
0.0139019
0.0556075
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101.6
62.17
89.94
91.6991
37.59
3.175
2
1
1
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82.71
62.1655
101.6,0|127,25.4|89.4616,76.3186|98.425,76.3186|115.957,77.6493|126.694,79.5166|136.965,83.2513|125.761,86.5192|115.257,88.6199|98.425,89.9414|53.8679,89.9414|32.6269,89.787|18.6218,89.0868|-1.21879,86.986|-19.192,83.2513|-0.751955,79.5166|19.322,77.4159|33.1427,76.1187|45.4876,76.2|63.5,25.4|0.0307977,0.290197|-95.25,0.00254|-120.65,4.2164|-190.5,4.2164|-215.9,-0.207876|0,0|
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10,10,10,10,10,10,10
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0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
128.148
Balsa
Custom Fin set
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196.85
0.491519
60.325
0.000803224
0.0032129
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120.65
65.44
4.22
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27.6
2.3876
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1
1
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95.5
65.4427
120.65,0|95.25,4.2164|25.4,4.2164|0,0|
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0.25,5,0.1,0.1,0.00018939,0.001,1
Estes
5.8967
924.265
Polyethylene LDPE
Parachute
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1
25.4
4.09187
38.1
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0
18 in
18 in plastic
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457.2
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6
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0.0254
457.2
1
0.00032972
Carpet String (Apogee 29500)
0.75
Custom
10.8862
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Mass object
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1
431.8
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25.4
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EST 3084
BT-5
95.25
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Semroc
1.13398
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Semroc
Simulated BNC-5AX Nose Cone
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1
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Semroc
Simulated BNC-5E Nose Cone
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BT-5
95.25
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Simulated BNC-5E Nose Cone
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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.
[C6-5]
14.6249
0.
0.
0.213333
1.83667
0.19
300.
0
Earth
Standard earth condistions.
0.219
35.7165
3.60899
0.891052
-3.49726
0,0,6.86333,0,0
-1,-1,-1,-1,-1
0,0,6.86333,0,0
32,32,80,32,32
1.
1
0.0885211
0.438722
0.00292665
1.94572e-05
40
1
0.
0.
1
212.847
3.4231
-15.7437
6.86333
128
1
C6
0.
Estes
6.35
0.
24
5.
87.4889
42.5751
136.346
4.35333
3.49
1
4.96352
86.2101
4
4.86333
2
0.863333
29.35
4.86333
0.850116
42.5689
0.346804
136.346
0.135962
4.76434
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.
[B6-4]
14.3381
0.
0.
0.213333
0.826667
0.173333
300.
0
Earth
Standard earth condistions.
0.11
4.76434
3.51298
0.244193
-3.50448
0,0,4.86333,0,0
-1,-1,-1,-1,-1
0,0,4.86333,0,0
32,32,80,32,32
1.
1
0.0836422
0.432869
0.00290646
1.78273e-05
40
1
0.
0.
1
86.2101
4.96352
-2.45279
4.86333
128
1
B6
0.
Estes
6.35
0.
24
4.
487.686
66.0485
105.158
10.9267
4.53333
1
7.10799
486.623
5
11.39
2
6.39333
146.477
11.39
1.12132
65.7305
0.76195
104.996
2.49993
63.1319
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.
[D3-5]
12.2692
0.
0.
0.186667
4.21667
0.316667
300.
0
Earth
Standard earth condistions.
0.453
3.18396
3.56569
0.206108
-3.55973
0,0,11.39,0,0
-1,-1,-1,-1,-1
0,0,11.39,0,0
32,32,80,32,32
1.
1
0.0903222
0.439756
0.00292404
2.16634e-05
40
1
0.
0.
1
486.623
7.10799
-63.1319
11.39
128
1
D3
0.
Apogee
6.35
0.
24
5.