4 Tomahawk Starfighter 1 1 1 0.75 0.8 0.81 0.95 0.95 1 0. 0. 0. 0. 0. 0. 0. 0. 4 914.4 0 0 0 1 0 Lester Anderson Version 2. 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Engine mount. 0. 0 -111.76 0. 0. 0. 0. 0. 0 57.9882 1.5708 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 0 -162.56 0 1 1 Semroc 1.09996 128.148 Balsa Nose cone 25.4 1 0. 3.82745 122.943 0.00719025 0.00719025 0. 0 BC-15044 Conical 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 rgb(206,211,255) white 1 4 1 0 0 rgb(0,0,0) 2. -0.0881278 2. -0.0881278 1 0 8 0 -162.56 111.76 40.386 1 0 0 25.4 0.127 0. 38.1 0. 0. 0. Estes 155.922 0. Estes lead weight 101.6 1 101.6 0. 0. 0. 0. 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 25 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 -60.96 0 0. Semroc 0. 848.979 Spiral/Glassine Engine tube 0. 0 111.76 24.3097 101.6 0.0257813 0.0257813 0. 0 LT-150300 Large Body 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 0 -50.8 40.386 38.1 203.2 0 0 0. 0.5 0. 0. 0 0 Semroc 0. 848.979 Spiral/Glassine Body tube 0. 0 -101.6 7.15181 88.9 0. 0. 0. 0 ST-9180 Body 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 8 1 0 2 blue 0. 0. 0. 0. 1 0 8 0 76.2 25.3492 24.13 177.8 0 1 24. 6.35 0. 0. 1 0 Estes 1.40047 0. Engine hook 123.825 1 123.825 0. 0. 0. 0. 0. 0 Engine hook Standard size 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 19 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 200.025 0 0. Semroc 0. 337.541 1/8 Aircraft Plywood Centering ring 0. 0 0. 0.680963 1.5875 0. 0. 0. 0 CR-913 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 0 149.225 38.1 25.3492 3.175 3 0 0 Semroc 0. 337.541 1/8 Aircraft Plywood Centering ring 0. 0 73.025 1.22183 1.5875 0. 0. 0. 0 CR-913 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 0 76.2 38.1 25.3492 3.175 3 0 0 Custom 0. 337.541 1/8 Aircraft Plywood Lower fins 0. 0 0. 4.32133 48.3023 0.00717741 0.00717741 0. 0 0. 2.61799 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 20 0 0 2 blue 11.7379 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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 13 1 0 0 blue 0. 0. 0. 0. 1 0 8 0 196.85 40.386 38.1 6.35 0 0 0. 0.5 0. 0. 0 0 Custom 0. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 1.06584 49.2963 0.00371577 0.00371577 0. 0 0. -0.261799 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 21 0 0 2 blue 2.89663 0.17964 3.35037 0.184492 1 0 8 0 152.4 1 101.6 29.69 25.4 28.753 22.48 1.5875 2 0 0 0. 0. 0. 1 0. 0. 33.6389 12.9448 0.292224 0. 0. 56.69 29.6872 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 1.06584 49.2963 0.00371577 0.00371577 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 22 0 0 2 blue 2.89663 0.17964 6.47242 0.184492 1 0 8 0 152.4 1 101.6 29.69 25.4 28.753 22.48 1.5875 2 0 0 0. 0. 0. 1 0. 0. 33.6389 12.9448 0.292224 0. 0. 56.69 29.6872 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 1.06584 49.2963 0.00371577 0.00371577 0. 0 0. 0.261799 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 2.89346 0.179792 9.1533 0.184337 1 0 8 0 152.4 1 101.6 28.02 25.4 28.7554 23.31 1.5875 2 0 0 0. 0. 0. 1 0. 0. 33.5296 12.9447 0.275787 0. 0. 57.26 28.0209 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 1.06584 49.2963 0.00371577 0.00371577 0. 0 0. 0.523599 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 2 blue 2.89346 0.179792 11.2105 0.184337 1 0 8 0 152.4 1 101.6 28.02 25.4 28.7554 23.31 1.5875 2 0 0 0. 0. 0. 1 0. 0. 33.5296 12.9447 0.275787 0. 0. 57.26 28.0209 101.6,0|47.625,25.4|0,6.35|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. 798.85 afterburner rear 0. 0 365.76 32.8245 22.2473 0.00530446 0.00530446 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(206,211,255) white 1 18 0 0 0 blue -3.21248 0.226667 -3.21248 0.226667 1 0 8 0 203.2 40.386 25.3746 50.8 0 0. 0. 1 12.7 0. 0. 0. 0 0. 136.674 85.8738 Custom 0. 337.541 1/8 Aircraft Plywood Right body plate 0. 0 -50.8 6.20613 93.3144 0.0103226 0.0103226 0. 0 0. -1.5708 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 43 1 0 0 blue 2.77733 -7.10543e-18 6.54082 0. 1 0 8 0 -50.8 1 203.2 203.2 25.4 25.4 0. 3.175 2 3 0 50.8 12.3952 0. 1 0. 0. 25.0952 7.55269 1. 0. 0. 203.2 203.2 203.2,0|203.2,25.4|0,25.4|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. 0. engine mount. Engine mount. 0. 0 -111.76 0. 0. 0. 0. 0. 0 57.9882 -1.5708 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 44 1 0 0 blue 0. 0. 0. 0. 1 0 8 0 -162.56 0 1 1 Semroc 1.09996 128.148 Balsa Nose cone 25.4 1 0. 3.82746 122.943 0.00719025 0.00719025 0. 0 BC-15044 Conical 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 rgb(206,211,255) white 1 45 1 0 0 rgb(0,0,0) 2. -0.0881278 2. -0.0881278 1 0 8 0 -162.56 111.76 40.386 1 0 0 25.4 0.127 0. 38.1 0. 0. 0. Estes 155.922 0. Estes lead weight 101.6 1 101.6 0. 0. 0. 0. 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 46 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 -60.96 0 0. Semroc 0. 848.979 Spiral/Glassine Engine tube 0. 0 111.76 24.3097 101.6 0.0257813 0.0257813 0. 0 LT-150300 Large Body 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 47 1 0 0 blue 0. 0. 0. 0. 1 0 8 0 -50.8 40.386 38.1 203.2 0 0 0. 0.5 0. 0. 0 0 Semroc 0. 848.979 Spiral/Glassine Body tube 0. 0 -101.6 7.15181 88.9 0. 0. 0. 0 ST-9180 Body 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 48 1 0 2 blue 0. 0. 0. 0. 1 0 8 0 76.2 25.3492 24.13 177.8 0 1 24. 6.35 0. 0. 1 0 Estes 1.40047 0. Engine hook 123.825 1 123.825 0. 0. 0. 0. 0. 0 Engine hook Standard size 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 49 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 200.025 0 0. Semroc 0. 337.541 1/8 Aircraft Plywood Centering ring 0. 0 0. 1.22183 1.5875 0. 0. 0. 0 CR-913 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 50 0 0 2 blue 0. 0. 0. 0. 1 0 8 0 149.225 38.1 25.3492 3.175 3 0 0 Semroc 0. 337.541 1/8 Aircraft Plywood Centering ring 0. 0 73.025 1.22183 1.5875 0. 0. 0. 0 CR-913 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 51 0 0 2 blue 0. 0. 0. 0. 1 0 8 0 76.2 38.1 25.3492 3.175 3 0 0 Custom 0. 337.541 1/8 Aircraft Plywood Lower fins 0. 0 0. 4.32133 48.3023 0.00717741 0.00717741 0. 0 0. -2.61799 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 52 0 0 2 blue 11.7844 0.110919 26.3876 0.111023 1 0 8 0 76.2 1 76.2 39.22 60.33 65.6309 44.33 3.175 2 0 0 69.85 6.35 3.175 1 0. 0. 47.1342 30.4698 0.514698 0. 0. 59.79 39.2174 76.2,0|88.9,25.4|76.2,50.8|50.8,60.325|0,50.8|25.4,50.8|25.4,25.4|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. 798.85 Afterburner front 0. 0 314.96 28.737 25.005 0.00465084 0.00465084 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(206,211,255) white 1 53 0 0 0 blue 3.21248 0.176316 3.21248 0.176316 1 0 8 0 152.4 25.3746 40.386 44.45 0 0. 0. 1 12.7 0. 0. 0. 0 0. 119.59 75.1396 Semroc 0. 848.979 Spiral/Glassine Afterburner 0. 0 359.41 0.759677 3.175 0.000805665 0.000805665 0. 0 LT-150300 Large Body 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 54 1 0 0 blue 0. 0. 0. 0. 1 0 8 0 196.85 40.386 38.1 6.35 0 0 0. 0.5 0. 0. 0 0 Custom 0. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 0.594641 44.8252 0.00207306 0.00207306 0. 0 0. -0.261799 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 55 0 0 2 blue 2.67331 0.179792 1.77897 0.184337 1 0 8 0 152.4 1 101.6 28.02 25.4 28.7554 23.31 1.5875 2 0 0 0. 0. 0. 1 0. 0. 22.9844 6.87341 0.275787 0. 0. 57.26 28.0209 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 0.594641 44.8252 0.00207306 0.00207306 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 56 0 0 2 blue 2.67331 0.179792 3.4367 0.184337 1 0 8 0 152.4 1 101.6 28.02 25.4 28.7554 23.31 1.5875 2 0 0 0. 0. 0. 1 0. 0. 22.9844 6.87341 0.275787 0. 0. 57.26 28.0209 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 0.594641 44.8252 0.00207306 0.00207306 0. 0 0. 0.261799 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 57 0 0 2 blue 2.67331 0.179792 4.86023 0.184337 1 0 8 0 152.4 1 101.6 28.02 25.4 28.7554 23.31 1.5875 2 0 0 0. 0. 0. 1 0. 0. 22.9844 6.87341 0.275787 0. 0. 57.26 28.0209 101.6,0|47.625,25.4|0,6.35|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. 361.377 1/16 Aircraft Plywood Cooling fin 0. 0 -50.8 1.06584 49.2963 0.00371577 0.00371577 0. 0 0. -0.523599 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 58 0 0 2 blue 2.89663 0.17964 1.11857e-06 0.184492 1 0 8 0 152.4 1 101.6 29.69 25.4 28.753 22.48 1.5875 2 0 0 0. 0. 0. 1 0. 0. 33.6389 12.9448 0.292224 0. 0. 56.69 29.6872 101.6,0|47.625,25.4|0,6.35|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. 798.85 afterburner rear 0. 0 365.76 32.8245 22.2473 0.00530446 0.00530446 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(206,211,255) white 1 59 0 0 0 blue -3.21248 0.226667 -3.21248 0.226667 1 0 8 0 203.2 40.386 25.3746 50.8 0 0. 0. 1 12.7 0. 0. 0. 0 0. 136.674 85.8738 Apogee 0. 1121.29 Paper Launch lug 0. 0 25.4 1.11647 38.1 0.00374649 0.0019944 0. 0 13056 16.5608 3.14159 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 60 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 25.4 8.3312 7.2644 76.2 0 DynaStar Mid-Power Rockets 0. 0. Polyethylene LDPE Parachute 0. 0 0. 2.1445 67.7501 0. 0. 0. 0 29117 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 61 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. 813.001 0. 8 8 0.024892 813.001 1 0.00032972 Carpet String (Apogee 29500) 0.75 926.75 142.743 454.689 11.3188 8.8025 1 37.3074 920.814 8 10.5163 0 2.51625 150.377 10.5163 0.925574 142.725 0.886982 116.687 21.3875 79.1846 0. 0. 0 914.4 0 0. 0 0. 0. 0. 759.813 0. 0. 50. 15. 0. 0. 0 2 0. 0.89408 2 0.01 0.02 0 5 0. 0.1 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. [F21W-8, F21W-8] 13.5006 0. 0. 0.13375 2.00125 10.5175 10 1 800. 0 Earth Standard earth condistions. 2.282 79.1846 0. 7.19816 0.886983 -7.1433 0. 0,0,10.5163,0,0 -1,-1,-1,-1,-1 0,0,10.5163,0,0 32,32,80,32,32 1. 1 0.672522 0.0633663 0.0111091 0.00014234 0.0960174 72.7788 1.31709 {f36a4eb6-7809-4602-83d2-0917258bf322} 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 61 1 0. 0. 1 920.814 37.3074 -19.3655 10.5163 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 F21W 0. Aerotech 6.35 0. 8 8. 0. 0. 1 F21W 0. Aerotech 6.35 0. 48 8. 0. 0. 1174.5 160.639 720.01 12.4 8.82 1 47.2389 1167.85 8 11.58 0 3.58 230.751 11.58 0.968529 160.568 0.89408 103.219 55.1307 132.71 0. 0. 0 914.4 0 0. 0 0. 0. 0. 759.813 0. 0. 50. 15. 0. 0. 0 2 0. 0.89408 2 0.01 0.02 0 5 0. 0.1 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. [F23-8, F23-8] 13.124 0. 0. 0.14875 2.88125 11.5813 10 1 800. 0 Earth Standard earth condistions. 1.672 132.71 0. 5.2779 0.63381 -5.23971 0. 0,0,11.58,0,0 -1,-1,-1,-1,-1 0,0,11.58,0,0 32,32,80,32,32 1. 1 0.695722 0.0636619 0.0108354 0.000252557 0.0960174 72.7788 1.30516 {45fae4a9-fccd-4403-b5e8-ed12c24b1888} 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 61 1 0. 0. 1 1167.85 47.2389 -43.4738 11.58 128 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 F23 0. Ellis Mountain Rocket Works 6.35 0. 8 8. 0. 0. 1 F23 0. Ellis Mountain Rocket Works 6.35 0. 48 8. 0. 0. 112.788 39.1943 85.7255 5.55875 3.9075 1 10.7682 106.95 5 6.65125 2 1.65125 27.0137 6.65125 1.52502 39.1584 0.723141 85.7255 0.0271153 9.15607 0. 0. 0 914.4 0 0. 0 0. 0. 0. 759.813 0. 0. 50. 15. 0. 0. 0 2 0. 0.89408 2 0.01 0.02 0 5 0. 0.1 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, D12-5] 11.0813 0. 0. 0.30375 1.62375 0.2825 10 1 800. 0 Earth Standard earth condistions. 0.343 4.80387 0. 5.23289 0.723145 -5.18268 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 0.629722 0.0549993 0.0104096 9.25384e-05 0.0960174 72.7788 1.6546 {6c132e90-abb6-4142-9210-6e1cb23242e1} 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 61 1 0. 0. 1 106.95 10.7682 -9.15607 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 6.35 0. 8 5. 0. 0. 1 D12 0. Estes 6.35 0. 48 5. 0. 0.