Clamp #	Clamp Seq	Total Curvature	Inplane Curvature	Out-of-Plane Curvature	Torsion
1	1	0.0112	0.0110	0.0020	-0.0155
2	2	0.0071	0.0064	0.0030	-0.0147
3	3	0.0122	0.0025	-0.0119	-0.0133
4	4	0.0430	-0.0035	-0.0428	-0.0113
5	5	0.0877	-0.0142	-0.0866	-0.0093
6	6	0.1403	-0.0237	-0.1382	-0.0042
7	7	0.2051	-0.0187	-0.2042	-0.0041
8	8	0.1979	0.0061	-0.1978	0.0035
9	9	0.1669	0.0155	-0.1662	0.0102
10	10	0.1187	0.0119	-0.1181	0.0154
11	11	0.0534	0.0086	-0.0527	0.0186
12	12	0.0303	0.0105	0.0284	0.0194
13	13	0.1109	0.0207	0.1089	0.0180
14.5	14	0.1468	0.0304	0.1436	0.0150
16	15	0.0539	0.0305	0.0444	0.0013
17	16	0.0300	0.0290	-0.0079	-0.0003
18	17	0.0486	0.0287	-0.0392	-0.0005
19	18	0.0574	0.0269	-0.0507	-0.0009
20	19	0.0608	0.0239	-0.0559	-0.0012
21	20	0.0629	0.0203	-0.0596	-0.0013
22	21	0.0590	0.0164	-0.0567	-0.0014
23	22	0.0491	0.0126	-0.0475	-0.0014
24	23	0.0347	0.0101	-0.0332	-0.0014
25	24	0.0187	0.0109	-0.0152	-0.0013
26	25	0.0163	0.0161	0.0021	-0.0011
27	26	0.0306	0.0255	0.0170	-0.0009
28	27	0.0464	0.0364	0.0288	-0.0006
29	28	0.0577	0.0448	0.0363	-0.0002
30	29	0.0580	0.0469	0.0342	0.0014
31	30	0.0451	0.0439	0.0102	0.0053
32	31	0.0640	0.0476	-0.0428	0.0078
33	32	0.1267	0.0676	-0.1072	0.0111
34	33	0.1513	0.0816	-0.1275	0.0117
35	34	0.1033	0.0633	-0.0816	0.0111
36	35	0.0443	0.0336	-0.0288	0.0124
37	36	0.0142	0.0140	0.0021	0.0105
38	37	0.0185	0.0010	0.0184	0.0089
39	38	0.0383	-0.0097	0.0371	0.0062
40	39	0.0861	-0.0177	0.0843	0.0034
41	40	0.1544	-0.0121	0.1539	-0.0057
42	41	0.1624	0.0091	0.1621	-0.0183
43	42	0.1109	0.0281	0.1073	-0.0231
44	43	0.0589	0.0399	0.0433	-0.0224
45	44	0.0554	0.0536	-0.0139	-0.0156
46	45	0.0693	0.0598	-0.0349	-0.0013
47	46	0.0206	0.0182	-0.0096	0.0157
48	47	0.0632	0.0268	-0.0572	0.0249
49	48	0.1272	0.1019	-0.0762	0.0293
50	49	0.0981	0.0965	-0.0173	0.0235
51	50	0.0687	0.0592	0.0348	0.0111
52	51	0.0800	0.0252	0.0759	-0.0064
53	52	0.1049	0.0334	0.0994	-0.0166
54	53	0.1133	0.0544	0.0994	-0.0261
55	54	0.0656	0.0225	0.0616	-0.0351
56	55	0.0219	-0.0082	0.0203	-0.0409
57	56	0.0240	-0.0222	-0.0092	-0.0433
58	57	0.0462	-0.0227	-0.0402	-0.0418
59	58	0.0805	-0.0177	-0.0786	-0.0369
60	59	0.1508	-0.0333	-0.1471	-0.0295
61	60	0.2098	-0.0638	-0.1999	-0.0187
62	61	0.1655	-0.0506	-0.1576	-0.0098
63	62	0.0681	-0.0071	-0.0678	0.0134
64	63	0.0215	0.0155	-0.0149	0.0499
65	64	0.0158	0.0067	-0.0144	0.0628
66	65	0.0220	-0.0112	-0.0190	0.0502
67	66	0.0216	-0.0201	-0.0080	0.0139
68	67	0.0243	-0.0213	0.0117	0.0200
69	68	0.0249	-0.0128	0.0214	0.0419
70	69	0.0177	-0.0002	0.0177	0.0511
71	70	0.0135	0.0113	0.0073	0.0456
72	71	0.0250	0.0216	0.0126	0.0260
73	72	0.0517	0.0353	0.0378	0.0030
74	73	0.0807	0.0536	0.0603	-0.0024
75	74	0.0989	0.0675	0.0723	-0.0023
76	75	0.1115	0.0679	0.0885	-0.0012
77	76	0.1222	0.0502	0.1115	-0.0010
78	77	0.1125	0.0230	0.1101	-0.0022
79	78	0.0655	0.0043	0.0653	-0.0041
80	79	0.0078	0.0073	-0.0027	-0.0048
81	80	0.0932	0.0431	-0.0826	-0.0070
82	81	0.1611	0.0816	-0.1389	-0.0034
83	82	0.1490	0.0701	-0.1315	-0.0103
84	83	0.0920	0.0341	-0.0854	-0.0051
85	84	0.0529	0.0123	-0.0514	-0.0051
86	85	0.0301	-0.0028	0.0299	-0.0030
87	86	0.1818	0.0005	0.1818	-0.0091
88	87	0.2023	0.0197	0.2013	-0.0015
89	88	0.1956	0.0161	0.1950	-0.0005
90	89	0.2169	-0.0112	0.2166	-0.0058
91	90	0.1691	-0.0186	0.1681	-0.0096
92	91	0.0686	-0.0047	0.0684	-0.0098
93	92	0.0291	0.0036	0.0289	-0.0126
94	93	0.0100	0.0100	0.0002	-0.0141
95	94	0.0188	0.0148	-0.0117	-0.0152
96	95	0.0172	0.0152	-0.0079	-0.0156