3 Blackhawk AGM-84 Standard ARM 1 0.75 0.8 0.81 0.95 0.95 1 0. 0. 0. 0. 0. 0. 0. 0. 1 914.4 0 0 0 1 0 Based on actual dimensions of completed model. Both sets of fins have thru the wall tabs to the motor tube as defined by the centering rings. The two sections of body tubes are coupled with a tube coupler and the tube coupler is glued to both. The original design called for a bulkhead 0.5 inches from the rear of the tube coupler with an eye bolt for shock cord connection, the coupler glued to the forward payload section and slip fit into the rear body tube. This design was not adapted as it allows approx. 8 inches of the side strake fins to be exposed when the payload section separates from the rear body tube. A U-bolt in the forward motor mount centering ring is used for shock cord retention via a quick link connector. Fins are beveled on all edges except where attached to body tube. Revised 1/21/06 - Change motor mount tube from 54mm to 38mm 1 26 1 0 CSV1|1|873.76,-9.9476e-14,0|700.656,-1841.33,-511.424|-0.169008,0.278485,-0.945454|1278,2730.21|30|2|1918.86|-8.22341|0|0|0|0 0,1377.81,0,0 0,18.7307,0,0 0,1407.51,0,0 0,25.543,0,0 0 1 0 1 0. 0. 0 0 0 0 5 0 0 0 0. 9.99998 9.99998 9.99998 9.99998 18 1 0. 0. 0 0. 0. 0. 0. -1 Public Missiles 283.495 1049.21 Polystyrene PS Nose cone 228.6 1 0. 389.499 320.204 0.0915715 0.0915715 0. 0 PNC-3.90 Plastic nose cone 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 1 0 0 0 blue 2. 0.198217 2. 0.198217 1 0 8 426.72 101.6 0 1 1 76.2 3.175 4.2 98.552 0. 0. 0. LOC/Precision 0. 1121.29 Paper Body tube 0. 0 0. 182.413 203.2 0.129717 0.129717 0. 0 LOC BT-3.9 Airframe tube 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 2 1 0 0 blue 0. 0. 0. 0. 1 0 8 101.6 99.06 406.4 0 0 0. 0.5 0. 0. 0 Public Missiles Ltd. 73.7088 1121.29 Paper Tube coupler 0. 1 317.5 93.1 88.9 0. 0. 0. 0 CT-3.90 Coupler tube 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 16 0 0 0 blue 0. 0. 0. 0. 1 0 8 99.06 96.012 177.8 0 4 1 LOC Precision 142. 0. Rip stop nylon Parachute 0. 1 127. 22.032 122.5 0. 0. 0. 0 LP-58 58 In. 16 lines 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 18 0 0 0 blue 0. 0. 0. 0. 1 0 8 1470. 0. 0 16 0.051054 1350. 1 0.00102 1/16 In. braided nylon 0.75 LOC/Precision 0. 1121.29 Paper Body tube 0. 0 0. 410.43 457.2 0.291864 0.291864 0. 0 LOC BT-3.9 Airframe tube 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 3 1 0 0 blue 0. 0. 0. 0. 1 0 8 101.6 99.06 914.4 0 0 0. 0.5 0. 0. 0 Custom 0. 344.269 1/4 Aircraft Plywood Fin set 0. 0 0. 158.085 83.4746 0.0289245 0.115698 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 14 0 0 2 blue 13.4032 1.64613 18.4981 1.64634 1 0 8 4 158.75 20.65 139.62 140.226 82.07 6.35 2 0 0 120.65 29.972 19.05 1 0. 104.37 20.645 158.75,0|133.352,108.294|63.583,139.619|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. 344.269 1/4 Aircraft Plywood Fin set 0. 0 228.6 341.204 466.693 0.0690939 0.276376 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 15 0 0 2 blue 3.32756 1.006 5.04488 1.01121 1 0 8 4 793.75 443.8 53.98 108.791 269.43 6.35 2 0 0 149.225 29.972 603.25 1 0. 636.36 443.8 793.75,0|742.811,53.8966|244.475,53.975|210.159,25.3884|31.6081,25.3884|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 Public Missiles 0. 8553.86 Brass Launch lug 0. 0 304.8 17.4265 76.2 0.00868415 0.00456037 0. 0 LL-0.38 55.5625 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 19 0 0 0 blue 0. 0. 0. 0. 1 0 8 9.525 8.5852 152.4 0 LOC/Precision 0. 1121.29 Paper Body tube 0. 0 457.2 98.5033 228.6 0. 0. 0. 0 LOC MMT-1.52 Motor mount tube 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 7 1 0 0 blue 0. 0. 0. 0. 1 0 8 41.656 38.608 457.2 0 1 38. 12.7 0. 0. 1 LOC Precision 0. 724.996 Aircraft plywood (LOC) Centering ring 0. 0 12.7 17.7405 1.5875 0. 0. 0. 0 LOC CR-3.9-2.14 Centering 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 blue white 1 8 0 0 2 blue 0. 0. 0. 0. 1 0 8 99.06 57.404 3.175 0 0 0 LOC Precision 0. 724.996 Aircraft plywood (LOC) Centering ring 0. 0 139.7 17.7405 1.5875 0. 0. 0. 0 LOC CR-3.9-2.14 Centering 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 blue white 1 9 0 0 2 blue 0. 0. 0. 0. 1 0 8 99.06 57.404 3.175 0 0 0 LOC Precision 0. 724.996 Aircraft plywood (LOC) Centering ring 0. 0 263.525 17.7405 1.5875 0. 0. 0. 0 LOC CR-3.9-2.14 Centering 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 blue white 1 10 0 0 2 blue 0. 0. 0. 0. 1 0 8 99.06 57.404 3.175 0 0 0 LOC Precision 0. 724.996 Aircraft plywood (LOC) Centering ring 0. 0 419.1 17.7405 1.5875 0. 0. 0. 0 LOC CR-3.9-2.14 Centering 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 blue white 1 11 0 0 2 blue 0. 0. 0. 0. 1 0 8 99.06 57.404 3.175 0 0 0 Public Missiles 76.5437 0. 6/7.5/11in. FNC Ubolt 419.1 1 419.1 0. 0. 0. 0. 0. 0 HDWE-UBOLT-SET Ubolt for FNCs 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 23 0 0 2 blue 0. 0. 0. 0. 1 0 8 0 0. LOC Precision 102.058 0.0167418 9/16 In. tubular nylon Shock cord 0. 1 0. 0. 0. 0. 0. 0. 2 SCTN-20 Tubular Nylon 9/16 In x 20 Ft 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 24 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 6096. 690.728 147.814 151.925 10.9638 8.7625 1 12.5717 683.408 10 12.2 2 2.20125 129.98 12.2 0.73671 147.441 3.47386 151.925 1.89234 295.796 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 3 1.34112 3.53163 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. [I211W-10] 14.9133 0. 0. 0.115 1.86125 0.00125 800. 0 Earth Standard earth condistions. 5.609 295.796 7.78589 3.47386 -6.96795 0,0,12.2,0,0 -1,-1,-1,-1,-1 0,0,12.2,0,0 32,32,80,32,32 1. 1 2.37982 1.12417 0.766195 0.0044995 18 1 0. 0. 1 683.408 12.5717 -65.3425 12.2 128 1 I211W 0. Aerotech 12.7 0. 7 10. 852.199 187.443 187.217 11.6 9.79875 1 4.37187 852.002 10 11.8 2 1.80125 144.347 11.8 0.547825 187.195 2.07928 187.217 2.15959 155.9 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 3 1.34112 3.53163 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. [I284W-10] 17.413 0. 0. 0.10125 1.565 0.00125 800. 0 Earth Standard earth condistions. 3.829 155.9 6.86487 1.34524 -6.73177 0,0,11.8,0,0 -1,-1,-1,-1,-1 0,0,11.8,0,0 32,32,80,32,32 1. 1 2.47132 1.1377 0.771209 0.00578316 18 1 0. 0. 1 852.002 4.37187 -54.0014 11.8 128 1 I284W 0. Aerotech 12.7 0. 7 10. 1033.18 220.209 257.242 12.2863 10.385 1 5.66036 1032.35 10 11.9 0 1.90125 201.48 11.9 0.387492 220.063 3.53138 257.242 5.26064 517.407 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 3 1.34112 3.53163 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. [J350W-10] 20.7937 0. 0. 0.08625 1.50375 0.00125 800. 0 Earth Standard earth condistions. 5.141 517.407 6.40141 3.53138 -5.33923 0,0,11.9,0,0 -1,-1,-1,-1,-1 0,0,11.9,0,0 32,32,80,32,32 1. 1 2.63925 1.16009 0.917669 0.00752365 18 1 0. 0. 1 1032.35 5.66036 -43.5006 11.9 128 1 J350W 0. Aerotech 12.7 0. 7 10.