3 Aerotech Cheetah 1 0.75 0.78 0.8 0.95 0.95 1 292. 0. 0. 0. 0. 527.05 0. 0. 4 914.4 1 1 0 2 0 Stock Aerotech Cheetah--Weights and CG are set in over-ride based on measured values - Design entered by G.A. Dean File from www.rocketreviews.com 4 196 1 0 01130000F0245C0200000000004D794000000000000000000000000000000000E62A8B7A26E18440F5F390F9CC9E7D40A4D8333918479240C17D582486AAB4BFF340E6EF7DC2ED3F51C04C9568F3D6BF64D4978AE2318B407B8A518FC96F9C400000000000003E400000000000000040 0,666.577,0,0 0,18.9147,0,0 0,679.907,0,0 0,23.6952,0,0 0 1 0 1 0. 0. 0 0 0 0 0 0 0 0 0. 10. 10. 10. 10. 9 1 0. 0. 0 0. 0. 0. 0. -1 Custom 0. 1049.21 Polystyrene PS Nose cone 0. 0 0. 33.5806 177.324 0.0235787 0.0235787 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. 0.10778 2. 0.10778 1 0 8 231.775 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. 37.8149 288.925 0.0876097 0.0876097 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 1 0 0 blue 0. 0. 0. 0. 1 0 8 48.26 46.99 577.85 1 0 0. 0. 0. 0. 0 Custom 0. 688.794 Cardboard Body tube 0. 0 409.575 4.81887 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 8 0 0 blue 0. 0. 0. 0. 1 0 8 29.9974 29.0068 152.4 3 1 29. 12.7 0. 0. 1 Custom 0. 1199.78 Polycarbonate Launch lug 0. 0 279.4 0.926499 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. 0 530.225 0.926499 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 0.0254 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 19.05 64.6904 72.5081 0.00970966 0.0388386 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 16.9147 0.73265 21.6952 0.73265 1 0 8 4 111.125 25.4 71.12 83.0376 85.725 3.175 0 1 2 0. 9.144 0. 1 0.879995 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 555.625 4.97224 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 46.99 29.9974 2.54 0 0 1 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 485.775 4.97224 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 46.99 29.9974 2.54 0 0 1 Custom 0. 1905.24 G10 fiberglass Ring 0. 0 409.575 9.94447 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 46.99 29.9974 5.08 0 0 1 344.14 77.8485 73.0794 8.7225 6. 1 9.55348,0,0,0,0,0,0,0,0,0 339.29,0,0,0,0,0,0,0,0,0 7,0,0,0,0,0,0,0,0,0 9.72,0,0,0,0,0,0,0,0,0 1 2.7225 0. 9.72 1.52577 77.8485 0. 73.0794 0. 0. 0. 0. 1.2192 0 0. 0 0. 760. 1.5708 50. 15. 0. 0 2 0. 1.29642 1 0. 0.02 0 6 1. 1. 1 0. 0 3 300. 2000. 1 6. 2 0.99 2000. 1500. 2 0.98 1 0. 0 0.08 1 0. 1 0. 1 0. [E15-7 ] 12.2791 0. 0. 0.21 2.38 0.04 400. 0 earth earth 1.20794 0. 0. 0. 0. 0,0,0 -1,-1,9.72 0,0,9.72 32,32,80 1. 5 0.3372 0.559854 0.0216254 8.46166e-05 9 1 0. 0. 1 339.29 9.55348 0. 9.72 7 1 E15 0. A-WL 12.7 0. 3 7. 394.679 108.233 145.291 8.41 7.18875 1 1.92568 394.502 7 8.22125 0 1.22125 86.2912 8.22125 0.653459 108.233 0.100854 145.291 0.0047504 2.28029 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] 16.0696 0. 0. 0.1225 1.07375 0.04125 800. 0 Earth Standard earth condistions. 4.921 2.28029 5.04489 0.100857 -5.04388 0,0,8.22125 -1,-1,8.22 0,0,8.22125 32,32,80 1. 1 0.3353 0.558655 0.0206092 7.55984e-05 9 1 0. 0. 1 394.502 1.92568 -0.0644263 8.22125 128 1 E30 0. Aerotech 12.7 0. 3 7. 622.202 137.283 152.022 10.105 7.425 1 5.35447 621.213 7 9.68 0 2.68 112.061 9.68 0.679718 137.281 0.696116 152.022 0.699457 44.6773 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] 15.6835 0. 0. 0.1175 1.74875 0.01 800. 0 Earth Standard earth condistions. 6.31 44.6773 5.59347 0.696121 -5.54999 0,0,9.68 -1,-1,9.68 0,0,9.68 32,32,80 1. 1 0.3666 0.5755 0.0192441 8.36217e-05 9 1 0. 0. 1 621.213 5.35447 -4.32026 9.68 128 1 F20EJ 0. Aerotech 12.7 0. 3 7. 536.191 123.349 140.269 9.62125 7.4 1 5.13157 535.306 7 9.22 0 2.22125 114.944 9.22 0.768524 123.329 0.792003 140.269 2.21324 50.5432 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] 14.8348 0. 0. 0.135 1.7675 0.03 800. 0 Earth Standard earth condistions. 6.41 50.5432 5.05748 0.370631 -5.04388 0,0,9.22 -1,-1,9.22 0,0,9.22 32,32,80 1. 1 0.3759 0.580188 0.0189141 8.5127e-05 9 1 0. 0. 1 535.306 5.13157 -11.777 9.22 128 1 F23FJ 0. Aerotech 12.7 0. 3 7. 663.448 135.783 138.457 10.77 8.08 1 8.91823 659.334 9 11.69 2 2.69 125.751 11.69 0.683621 135.762 0.89408 138.457 0.389891 83.1055 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] 15.6067 0. 0. 0.135 1.89875 0.04 800. 0 Earth Standard earth condistions. 6.972 83.1055 5.58007 0.779454 -5.52537 0,0,11.69 -1,-1,11.69 0,0,11.69 32,32,80 1. 1 0.3892 0.584628 0.0203987 0.000133872 9 1 0. 0. 1 659.334 8.91823 -15.5223 11.69 128 1 F25 0. Aerotech 12.7 0. 3 9. 573.001 121.007 87.8356 10.4413 7.83125 1 11.137 566.429 9 11.61 2 2.61 112.644 11.61 1.10048 120.979 0.89408 87.8356 0.419328 70.6107 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] 12.3273 0. 0. 0.1675 2.18 0.04125 800. 0 Earth Standard earth condistions. 6.023 70.6107 5.57482 0.786534 -5.51905 0,0,11.61 -1,-1,11.61 0,0,11.61 32,32,80 1. 1 0.3927 0.586169 0.0203386 0.000136223 9 1 0. 0. 1 566.429 11.137 -16.9346 11.61 128 1 F26FJ 0. Aerotech 12.7 0. 3 9. 525.52 129.002 176.971 9.55 8.07875 1 0.901687 525.49 8 9.47 1 1.47125 105.159 9.47 0.546339 129. 0.388753 176.971 0.150674 14.5316 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] 17.4167 0. 0. 0.1075 1.1775 0.01 800. 0 Earth Standard earth condistions. 5.714 14.5316 5.45098 0.0513394 -5.45074 0,0,9.47 -1,-1,9.47 0,0,9.47 32,32,80 1. 1 0.368 0.576221 0.0208373 0.000106703 9 1 0. 0. 1 525.49 0.901687 -4.65191 9.47 128 1 F42T 0. Aerotech 12.7 0. 3 8. 683.456 180.097 216.541 10.1838 8.7525 1 2.40511 683.158 9 10.43 2 1.43125 143.854 10.43 0.457424 180.097 0.255697 216.541 0.0140322 9.83039 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] 19.5955 0. 0. 0.1 1.1325 0.01375 800. 0 Earth Standard earth condistions. 7.731 9.83039 5.05036 0.255702 -5.04388 0,0,10.43 -1,-1,10.43 0,0,10.43 32,32,80 1. 1 0.3818 0.581279 0.0187508 9.11424e-05 9 1 0. 0. 1 683.158 2.40511 -0.280923 10.43 128 1 F50T 0. Aerotech 12.7 0. 3 9. 773.525 159.387 122.663 10.4013 7.76125 1 19.7066 769.203 7 9.64 0 2.64 146.65 9.64 0.823927 159.385 0.847306 116.787 2.59638 78.833 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] 14.3405 0. 0. 0.13875 2.1525 9.64125 800. 0 Earth Standard earth condistions. 7.382 78.833 5.65428 0.847309 -5.59043 0,0,9.64 -1,-1,9.64 0,0,9.64 32,32,80 1. 1 0.4184 0.592762 0.0198967 0.000199191 9 1 0. 0. 1 769.203 19.7066 -5.30083 9.64 128 1 G38FJ 0. Aerotech 12.7 0. 3 7. 929.098 211.602 204.827 11.4925 9.1925 1 7.83506 925.927 10 12.3 2 2.3 191.752 12.3 0.504975 211.584 0.754417 204.827 0.80678 56.075 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] 18.4653 0. 0. 0.10875 1.77 0.025 800. 0 Earth Standard earth condistions. 9.436 56.075 5.04427 0.0623378 -5.04388 0,0,12.3 -1,-1,12.3 0,0,12.3 32,32,80 1. 1 0.415 0.591519 0.0182548 0.000124166 9 1 0. 0. 1 925.927 7.83506 -14.458 12.3 128 1 G40W 0. Aerotech 12.7 0. 3 10. 913.321 245.084 316.266 11.0763 9.665 1 3.2605 912.773 10 11.41 2 1.41125 188.595 11.41 0.323175 245.083 0.798642 316.266 0.0747572 79.4948 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] 22.9609 0. 0. 0.085 1.15375 0.01625 800. 0 Earth Standard earth condistions. 9.307 79.4948 5.10672 0.798645 -5.04388 0,0,11.41 -1,-1,11.41 0,0,11.41 32,32,80 1. 1 0.4081 0.588934 0.0183269 0.000118069 9 1 0. 0. 1 912.773 3.2605 -1.04568 11.41 128 1 G80T 0. Aerotech 12.7 0. 3 10.