3 Aerotech Mustang 1 0.75 0.78 0.8 0.95 0.95 1 311.845 0. 0. 0. 0. 0. 0. 0. 4 914.4 0 1 0 2 0 Stock Aerotech Mustang--Weights are not accurate--11oz has been specified as the weight. Design entered by Andy Tate Original RockSim file from www.RocketReviews.com 4 15 1 0 01000000000000000000000000477C40000000000000000000000000000000000000000000477C40000000000000000000000020900CA6400000000000000000000000000000F03F000000000000000085EB912BEEF3A3405C8FE21CB0BDA8400000000000003E400000000000000040 0,771.665,0,0 0,32.5441,0,0 0,778.798,0,0 0,39.45,0,0 0 1 0 1 0. 0. 0 0 0 0 0 0 0 0 0. 10. 9.99998 9.99998 9.99998 9 1 0. 0. 0 0. 0. 0. 0. -1 Custom 0. 1049.21 Polystyrene PS Nose cone 0. 0 0. 42.8313 233.577 0.0325223 0.0325223 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 1 0 0 0 blue 2. 0.149372 2. 0.149372 1 0 8 320.675 48.26 1 1 1 50.8 1.016 0. 45.72 0. 0. 0. Custom 0. 688.794 Cardboard Body tube 0. 0 0. 75.4414 292.1 0.0885725 0.0885725 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 2 0 0 0 blue 0. 0. 0. 0. 1 0 8 48.26 45.72 584.2 1 0 0. 12.7 0. 0. 0 Custom 0. 688.794 Cardboard Body tube 0. 0 409.575 4.81594 76.2 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 3 0 0 0 blue 0. 0. 0. 0. 1 0 8 29.997 29.007 152.4 3 1 29. 12.7 0. 0. 1 Custom 0. 1199.78 Polycarbonate Launch lug 0. 0 279.4 0.926497 12.7 0.0012465 0.00070939 0. 0 28.575 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 0 0 0 blue 0. 0. 0. 0. 1 0 8 8.89 6.35 25.4 1 Custom 0. 1199.78 Polycarbonate Launch lug 0. 0 536.575 0.926497 12.7 0.0012465 0.00070939 0. 0 28.575 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 0 blue 0. 0. 0. 0. 1 0 8 8.89 6.35 25.4 1 Custom 0. 0.006685 Rip stop nylon Parachute 0. 0 165.1 24.5085 46.5667 0. 0. 0. 1 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 0 blue 0. 0. 0. 0. 1 0 8 558.8 0. 0 6 0.025 558.8 1 0.00242 5/64 In. round elastic 0.75 Custom 0. 0.00402 1/4 In. flat elastic Mass object 0. 0 257.175 7.35178 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 10 0 0 0 blue 0. 0. 0. 0. 1 0 8 1 1828.8 Custom 28.35 0. Inside Fins 0. 1 485.775 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 11 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. Custom 2.835 0. Motor Hook 0. 1 565.15 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 12 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. Custom 28.35 0. Eye Screw and Baffle 0. 1 409.575 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 13 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. Custom 56.699 0. Cooling Mesh 0. 1 444.5 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 14 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. Custom 0. 1049.21 Polystyrene PS Fin set 0. 0 412.75 130.67 107.694 0.0196129 0.0784515 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 0 blue 30.5441 0.812412 37.45 0.812412 1 0 8 4 165.1 38.1 96.52 115.547 127.022 3.175 0 1 2 0. 0. 0. 1 0.92 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 555.625 4.52483 1.27 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 4 0 0 0 blue 0. 0. 0. 0. 1 0 8 45.72 29.997 2.54 0 0 1 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 485.775 4.52483 1.27 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 5 0 0 0 blue 0. 0. 0. 0. 1 0 8 45.72 29.997 2.54 0 0 1 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 409.575 9.04966 2.54 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 6 0 0 0 blue 0. 0. 0. 0. 1 0 8 45.72 29.997 5.08 0 0 1 243.737 60.4918 70.7823 7.705 5.065 1 17.6029 226.022 7 9.64 2 2.64 46.3125 9.64 1.98445 60.4827 0.275779 70.7823 0.102064 7.43215 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [E15-7] 9.39985 0. 0. 0.2025 2.31125 9.64125 800. 0 Earth Standard earth condistions. 6.93 0.0755238 6.06395 0.139109 -6.06236 0,0,9.64 -1,-1,9.64 0,0,9.64 32,32,80 1. 1 0.471905 0.710946 0.0272955 0.000163002 9 1 0. 0. 1 226.022 17.6029 -7.43215 9.64 128 1 E15 0. Aerotech 12.7 0. 3 7. 258.608 75.3686 99.644 7.26 6.03875 1 9.28245 254.114 7 8.22125 2 1.22125 40.0612 8.22125 0.958783 75.3653 0.642288 99.644 0.0831139 14.3607 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [E30-7] 13.2517 0. 0. 0.14625 1.08375 0.04125 800. 0 Earth Standard earth condistions. 9.233 14.3607 7.9607 0.642293 -7.93475 0,0,8.22125 -1,-1,8.22 0,0,8.22125 32,32,80 1. 1 0.465105 0.708761 0.0274959 0.000162895 9 1 0. 0. 1 254.114 9.28245 -3.96416 8.22125 128 1 E30 0. Aerotech 12.7 0. 3 7. 450.454 99.1661 105.523 9.37875 6.69875 1 2.95163 450.007 7 9.68 2 2.68 68.3162 9.68 0.985164 99.1658 0.315353 105.523 0.0302645 10.1826 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F20EJ-7] 12.9777 0. 0. 0.14125 1.8275 0.01 800. 0 Earth Standard earth condistions. 9.184 10.1826 7.71979 0.315358 -7.71335 0,0,9.68 -1,-1,9.68 0,0,9.68 32,32,80 1. 1 0.496405 0.717343 0.0268897 0.000170918 9 1 0. 0. 1 450.007 2.95163 -1.60781 9.68 128 1 F20EJ 0. Aerotech 12.7 0. 3 7. 374.198 88.0203 97.4027 8.7475 6.52625 1 4.77426 373.102 7 9.22 2 2.22125 70.3062 9.22 1.12889 88.001 0.698437 97.4027 0.238649 23.794 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F23FJ-7] 12.1949 0. 0. 0.16 1.825 0.03 800. 0 Earth Standard earth condistions. 9.384 23.794 6.07837 0.440955 -6.06236 0,0,9.22 -1,-1,9.22 0,0,9.22 32,32,80 1. 1 0.505705 0.719853 0.0267373 0.000172424 9 1 0. 0. 1 373.102 4.77426 -11.2486 9.22 128 1 F23FJ 0. Aerotech 12.7 0. 3 7. 537.082 113.591 115.446 10.0088 7.31875 1 15.5517 523.632 9 11.69 2 2.69 77.3187 11.69 0.831127 113.575 0.595127 115.446 0.280636 15.9031 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F25-9] 14.2138 0. 0. 0.14625 1.9125 0.04 800. 0 Earth Standard earth condistions. 10.385 15.9031 7.94373 0.306995 -7.9378 0,0,11.69 -1,-1,11.69 0,0,11.69 32,32,80 1. 1 0.519005 0.721882 0.0266113 0.000181933 9 1 0. 0. 1 523.632 15.5517 -13.7093 11.69 128 1 F25 0. Aerotech 12.7 0. 3 9. 455.528 100.32 72.6576 9.6425 7.0325 1 17.8236 437.263 9 11.61 2 2.61 82.575 11.61 1.33538 100.319 0.100325 72.6576 0.0618369 3.32194 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F26FJ-9] 11.1675 0. 0. 0.1825 2.185 0.04125 800. 0 Earth Standard earth condistions. 11.597 -1.00098 6.06236 0.000156646 -6.06236 0,0,11.61 -1,-1,11.61 0,0,11.61 32,32,80 1. 1 0.522505 0.722716 0.0266147 0.000184822 9 1 0. 0. 1 437.263 17.8236 -3.32194 11.61 128 1 F26FJ 0. Aerotech 12.7 0. 3 9. 411.03 104.863 143.335 8.74 7.26875 1 7.08923 408.429 8 9.47 2 1.47125 65.9312 9.47 0.670909 104.862 0.237101 143.335 0.0819759 4.53819 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F42T-8] 15.7581 0. 0. 0.12 1.1825 0.01 800. 0 Earth Standard earth condistions. 9.544 4.53819 7.09557 0.0584994 -7.09533 0,0,9.47 -1,-1,9.47 0,0,9.47 32,32,80 1. 1 0.497805 0.717726 0.0268001 0.000169413 9 1 0. 0. 1 408.429 7.08923 -3.34319 9.47 128 1 F42T 0. Aerotech 12.7 0. 3 8. 519.733 130.338 151.996 9.5375 8.10625 1 8.65598 515.856 9 10.43 2 1.43125 75.1612 10.43 0.639493 130.324 0.858045 151.996 0.343814 39.6133 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [F50T-9] 16.2583 0. 0. 0.1175 1.1525 0.01375 800. 0 Earth Standard earth condistions. 11.146 39.6133 7.92596 0.668868 -7.89769 0,0,10.43 -1,-1,10.43 0,0,10.43 32,32,80 1. 1 0.511605 0.720082 0.0266699 0.000178439 9 1 0. 0. 1 515.856 8.65598 -10.5526 10.43 128 1 F50T 0. Aerotech 12.7 0. 3 9. 651.266 136.555 100.183 10.3425 7.7025 1 12.282 648.121 7 9.64 0 2.64 92.2925 9.64 0.956066 136.555 0.473343 100.183 0.605163 22.0507 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [G38FJ-7] 13.2091 0. 0. 0.14875 2.1575 0.025 800. 0 Earth Standard earth condistions. 12.568 22.0507 7.84706 0.473348 -7.83277 0,0,9.64 -1,-1,9.64 0,0,9.64 32,32,80 1. 1 0.548205 0.725514 0.026499 0.00021756 9 1 0. 0. 1 648.121 12.282 -2.26064 9.64 128 1 G38FJ 0. Aerotech 12.7 0. 3 7. 751.181 160.156 146.194 11.155 8.855 1 10.9437 744.819 10 12.3 2 2.3 132.797 12.3 0.69268 160.156 0.230755 146.194 0.0103426 8.1983 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [G40W-10] 15.5829 0. 0. 0.1275 1.85875 0.025 800. 0 Earth Standard earth condistions. 20.88 8.1983 6.06675 0.23076 -6.06236 0,0,12.3 -1,-1,12.3 0,0,12.3 32,32,80 1. 1 0.544805 0.724841 0.0264752 0.000211462 9 1 0. 0. 1 744.819 10.9437 -0.343556 12.3 128 1 G40W 0. Aerotech 12.7 0. 3 10. 749.258 182.416 226.081 10.7938 9.3825 1 6.03608 747.404 10 11.41 2 1.41125 132.535 11.41 0.450328 182.406 0.729744 226.081 0.464365 48.2246 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 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 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [G80T-10] 19.434 0. 0. 0.1 1.18625 0.01625 800. 0 Earth Standard earth condistions. 21.511 48.2246 6.06644 0.222359 -6.06236 0,0,11.41 -1,-1,11.41 0,0,11.41 32,32,80 1. 1 0.537905 0.72345 0.0265055 0.000205365 9 1 0. 0. 1 747.404 6.03608 -9.94079 11.41 128 1 G80T 0. Aerotech 12.7 0. 3 10.