3 SHR 1/48th Scale Saturn V 1 0.9 0.78 0.8 0.95 0.95 1 3855.54 0. 0. 0. 0. 1087.12 0. 0. 4 1220.42 1 1 0 2 0 Note: The reference diameter is set to use the maximum frontal area. But even so, RockSim will always tell you if the rocket will be stable by looking at the 2D flight profile. Tim Van Milligan. Visit my web site at: www.ApogeeRockets.com Dimensions may not be 100% accurate. Please check them yourself! 4 215 1 0 CSV1|1|989.013,-1.13687e-13,0|1961.48,-191.384,-530.836|-0.0478496,0.908474,-0.415193|36.2944,3629.44|30|2|1124.33|22.7903|0|0|0|0 0,1280.79,0,0 0,25.3717,0,0 0,1353.45,0,0 0,28.3199,0,0 0 1 0 1 0. 0. 0 0 0 0 3 0 0 1 0. 9.99998 10.0076 10.0076 10.0076 213 1 0. 0. 0 0. 0. 0. 0. -1 215 1 0. 0. 0 0. 0. 0. 0. -1 Custom 0. 1185.37 Acrylic (Cast) Nose cone 0. 0 0. 45.6902 69.6162 0.0115385 0.0115385 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(255,255,255) white 1 1 0 0 0 rgb(0,0,0) 2. 0.0465201 2. 0.0465201 1 0 8 69.85 88.9 0 0 0 12.7 0.762 0. 54.7624 0. 0. 0. Custom 92. 0. 92g clay nose mass 0. 1 28.575 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 60 0 0 0 blue 0. 0. 0. 0. 1 0 8 0 0. uline 0. 1121.29 Paper Service Module Body tube (Front Part) 0. 0 0. 37.3413 47.625 0.0266021 0.0266021 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(179,179,179) white 1 2 1 0 0 rgb(51,51,51) 0. 0. 0. 0. 1 0 8 88.9 86.36 95.25 0 0 0. 0. 0. 0. 0 Custom 0. 1121.29 Paper Transition (LEM area) 0. 0 0. 23.5256 96.6385 0.0636547 0.0636547 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(255,255,255) white 1 3 1 0 0 rgb(128,0,64) 2.5 0.26162 2.5 0.26162 1 0 8 88.9 133.35 180.975 0 0. 0. 1 0.3302 0. 0. 0. 0 0. 542.925 361.95 Uline 0. 1121.29 Paper 3rd Stage tube (front portion) 0. 0 0. 397.54 136.525 0.114389 0.114389 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(255,255,255) white 1 5 1 0 0 rgb(0,0,128) 0. 0. 0. 0. 1 0 8 133.35 127. 273.05 0 0 0. 0. 0. 0. 0 Dynastar 0. 0.006685 Rip stop nylon Parachute 0. 0 412.75 109.788 127. 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 rgb(255,128,0) white 1 215 0 0 0 rgb(255,128,0) 0. 0. 0. 0. 1 0 8 1524. 0. 8 8 0. 0. 1 0.00102 1/16 In. braided nylon 0.75 Custom 0. 1049.21 Polystyrene PS 2nd to 3rd stage Transition 0. 0 0. 41.4432 75.04 0.077899 0.077899 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(230,230,230) white 1 80 1 0 0 rgb(0,64,128) 6.61224 0.694149 6.61224 0.694149 1 0 8 133.35 209.55 139.7 0 0. 0. 1 0.508 0. 0. 0. 0 0. 384.175 244.475 Uline 0. 1121.29 Paper Main Body Tube 0. 0 0. 2814.13 609.6 0.802625 0.802625 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(255,255,255) white 1 82 1 0 0 rgb(0,0,0) 0. 0. 0. 0. 1 0 8 209.55 203.2 1219.2 0 0 0. 0. 0. 0. 0 Custom 0. 344.269 1/4 Aircraft Plywood Forward motor tube centering disk 0. 0 381. 65.4129 3.175 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 rgb(0,128,64) white 1 87 0 0 0 rgb(0,128,0) 0. 0. 0. 0. 1 0 8 203.2 56.5 6.35 3 0 1 Custom 0. 344.269 1/4 Aircraft Plywood Rear motor tube centering disk 0. 0 1168.4 65.4129 3.175 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 rgb(0,128,64) white 1 91 0 0 0 rgb(0,128,0) 0. 0. 0. 0. 1 0 8 203.2 56.5 6.35 0 0 1 Custom 0. 1049.21 Polystyrene PS Custom Fin set 0. 0 0. 154.825 112.186 0.0154511 0.0618046 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(255,255,255) white 1 92 0 0 2 rgb(128,0,128) 14.2595 1.90461 17.2076 1.91732 1 0 8 4 159.85 73.97 109.88 138.584 127.39 4.7752 2 0 1 0. 0. 0. 0 0. 70.53 73.9686 159.852,0|159.335,37.2236|148.169,37.2352|148.245,109.875|116.134,109.875|66.3213,17.9285|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. 958.705 Kraft phenolic motor mount 1 0. 0 330.2 179.635 431.8 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 1 211 0 0 0 blue 0. 0. 0. 0. 1 0 8 56.5 54. 863.6 0 1 54. 12.7 0. 0. 1 DYNASTAR 0. 0.006685 Rip stop nylon Parachute 0. 0 330.2 102.591 122.767 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 rgb(255,128,0) white 1 213 0 0 0 rgb(255,128,0) 0. 0. 0. 0. 1 0 8 1473.2 0. 8 8 0. 0. 2 0.00102 1/16 In. braided nylon 0.75 89.1542 36.0365 44.3851 4.76125 3.35 1 6.32391 87.0943 4 5.41125 2 1.41125 17.5213 5.41125 2.35158 36.0307 0.58427 44.3851 0.0282533 4.08757 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 2 0. 0.89407 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-4, G80T-4] 8.461 0. 0. 0.2225 1.19375 0.01625 800. 0 Earth Standard earth condistions. 0.406 4.08757 7.22681 0.531874 -7.20721 0,0,5.41125 -1,-1,5.41 0,0,5.41125 32,32,80 1. 1 4.08774 1.13346 1.61961 0.0336733 214 1 0. 0. 1 87.0943 6.32391 -2.67232 5.41125 128 213 1 0. 0. 0 0. 0. 0. 0. -1 1 G80T 0. Aerotech 12.7 0. 211 4. 1 G80T 0. Aerotech 12.7 0. 212 4. 89.1036 36.0315 44.3851 4.76 3.34875 1 6.37227 87.034 4 5.41125 2 1.41125 21.8387 5.41125 2.35153 36.0184 0.892936 44.3851 0.0432429 10.7462 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 2 0. 0.89407 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-4, G80T-4] 8.461 0. 0. 0.2225 1.19375 0.01625 800. 0 Earth Standard earth condistions. 0.453 10.7462 5.34492 0.881731 -5.27169 0,0,5.41125 -1,-1,5.41 0,0,5.41125 32,32,80 1. 1 4.08774 1.13346 1.52419 0.0337494 213 1 0. 0. 1 87.034 6.37227 -3.84677 5.41125 128 215 1 0. 0. 0 0. 0. 0. 0. -1 1 G80T 0. Aerotech 12.7 0. 211 4. 1 G80T 0. Aerotech 12.7 0. 212 4. 89.2049 36.0416 44.3851 4.76375 3.3525 1 6.27681 87.1563 4 5.41125 2 1.41125 21.8625 5.41125 2.35162 36.0416 0.0145673 44.3851 0.00133378 0.138784 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 2 0. 0.89407 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-4, G80T-4] 8.46101 0. 0. 0.2225 1.19375 0.01625 800. 0 Earth Standard earth condistions. 0.313 -0.0199028 5.27169 0.00186956 -5.27169 0,0,5.41125 -1,-1,5.41 0,0,5.41125 32,32,80 1. 1 4.08774 1.13346 1.53627 0.0337515 213 1 0. 0. 1 87.1563 6.27681 -0.138784 5.41125 128 215 1 0. 0. 0 0. 0. 0. 0. -1 1 G80T 0. Aerotech 12.7 0. 211 4. 1 G80T 0. Aerotech 12.7 0. 212 4. 89.2033 36.0415 44.3851 4.76375 3.3525 1 6.27905 87.1543 4 5.41125 2 1.41125 18.35 5.41125 2.35162 36.0412 0.0835352 44.3851 0.00622903 0.643929 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 2 0. 0.89407 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-4, G80T-4] 8.46101 0. 0. 0.2225 1.19375 0.01625 800. 0 Earth Standard earth condistions. 0.281 0.232539 6.74197 0.0530025 -6.74176 0,0,5.41125 -1,-1,5.41 0,0,5.41125 32,32,80 1. 1 4.08774 1.13346 1.53627 0.0337515 213 1 0. 0. 1 87.1543 6.27905 -0.643929 5.41125 128 215 1 0. 0. 0 0. 0. 0. 0. -1 1 G80T 0. Aerotech 12.7 0. 211 4. 1 G80T 0. Aerotech 12.7 0. 212 4. 454.495 74.9713 22.5427 12.0063 3.745 0 4 8.26125 22.6025 0. 5.23927 67.0907 0. 22.5423 0.0635798 8.03404 0. 0. 914.4 0 0. 0 0. 759.813 1.571 50. 15. 0. 0 2 0. 0.89407 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. [I65W-None] 5.28389 0. 0. 0.45 22.6012 1.72375 800. 0 Earth Standard earth condistions. 0.5 -8.03404 74.9758 -0.242292 -74.9754 0,0,0 -1,-1,1.6e+308 0,0,0 32,32,32 1. 1 4.63164 1.21457 1.63611 0.036504 213 1 0. 0. 0 0. 0. 0. 0. -1 215 1 0. 0. 0 0. 0. 0. 0. -1 1 I65W 0. Aerotech 12.7 0. 211 -2.