3
Dr. Zooch Discoverer Thor
1
1
1
0.75
0.8
0.81
0.95
0.95
1
62.
0.
0.
0.
0.
206.299
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914.4
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Finished rocket weighed and measured in launch configuration. CG was found by suspension from a string loop at exactly 0.50 inches from the front of the main T-60 tube, or 9.50 inches from the nose tip. The RockSim file has been modified using the CG override to reflect the measured CG, and the all up weight of my model (101 grams ready to launch) has been programmed using mass override. The CP calculation is set to the Barrowman calculation to reflect a more conservative 'worst case'. The nose cone and transition had to be similated in RockSim as two seperate components to get the round tip on the nose cone and the compound transition to appear correctly (as if they were two seperate parts glued together).
Dr. Zooch Discoverer Thor, RockSim file by Jeff Roberts as measured from DT kit built 5/30/08 per instructions with virtually no modifications. Rocket was constructed using standard materials and methods. Only deviations from the instructions were the use of blue painters tape instead of electrical tape in the motor hook attachment, and CA hardening of the nose cone and transition. Fins were encased in regular printer paper using wood glue and sanded to a rounded leading edge before encasement. Rocket was finished using Elmers Sanding Wood Filler on the nosecone and transition after CA hardening and is virtually identical to the rocket in the EMRR review visually. No black band around the T-60 was used. Filled and sanded rocket was primed and sanded then wet sanded. Paint was low gloss white and the standard kit wrap on the upper stage T-50 and trim pieces per the kit on the transition and T-60 Thor body tube. Nozzle constructed per kit instructions, except the use of small paper tabs to align the upper/lower halves. Rocksim does not allow it to be showed recessed on the motor tube as it is supposed to be.
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0.75
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7.087
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1/4 In. flat elastic
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2.2352
157.281
3.68402
52.2887
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
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.
[C6-5]
15.0791
0.
0.
0.2125
1.8375
0.19125
10
1
800.
0
Earth
Standard earth condistions.
1.457
52.2887
0.
5.59517
2.2352
-5.1293
0.
0,0,6.86125,0,0
-1,-1,-1,-1,-1
0,0,6.86125,0,0
32,32,80,32,32
1.
1
0.0851
0.247892
0.00175164
2.45904e-05
{ff0c5567-3d8f-48b1-a822-0cc1d6e24b33}
0
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
0
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
18
1
0.
0.
1
227.765
6.75937
-47.038
6.86125
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
C6
0.
Estes
12.7
0.
12
5.
0.
0.
473.276
161.683
273.932
7.95125
6.55
1
6.29772
472.282
7
8.40125
2
1.40125
97.2575
8.40125
0.419969
160.969
2.2352
273.932
6.1946
145.931
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
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.
[D10-7]
19.9339
0.
0.
0.09625
1.10125
0.01875
10
1
800.
0
Earth
Standard earth condistions.
2.731
145.931
0.
5.71416
2.2352
-5.25885
0.
0,0,8.40125,0,0
-1,-1,-1,-1,-1
0,0,8.40125,0,0
32,32,80,32,32
1.
1
0.0879
0.251448
0.00181521
2.55256e-05
{529ffa8f-2297-4ee2-9e1f-211ccac5e9c3}
0
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
0
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
18
1
0.
0.
1
472.282
6.29772
-52.6803
8.40125
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
D10
0.
Apogee
12.7
0.
12
7.
0.
0.
487.68
187.324
359.454
7.8525
6.91125
1
3.58402
487.64
7
7.94125
2
0.94125
100.309
7.94125
0.283192
186.85
2.2352
359.454
6.38917
167.952
0.
0.
0
914.4
0
0.
0
0.
0.
0.
759.813
0.
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.
[D21T-7]
24.7467
0.
0.
0.09
0.81375
0.03
10
1
800.
0
Earth
Standard earth condistions.
2.769
167.952
0.
5.69243
2.2352
-5.23523
0.
0,0,7.94125,0,0
-1,-1,-1,-1,-1
0,0,7.94125,0,0
32,32,80,32,32
1.
1
0.087
0.25033
0.00179513
2.5225e-05
{fe8bf5e3-ddca-4140-80fe-2b1175c78f73}
0
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
0
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
18
1
0.
0.
1
487.64
3.58402
-38.5076
7.94125
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
D21T
0.
Aerotech
12.7
0.
12
7.
0.
0.