# RCCAD File Format V 1.7.1 1 Wing Type 16 50 140 140 .23 .21 400 -5 -2 -3 70 200 200 200 Wing Type 16 50 150 100 .13 .13 210 30 50 50 760 200 200 200 Wing Type 16 48.5 150 150 .16 .15 450 0 -1 -1 71 47 47 47 2 Fuselage 12 16 0 0 0 #FALSE# #TRUE# #TRUE# 200 200 200 0 0 0 7 1.17 1.17 .88 5 13.1061580625314 22.4676995357682 6 1.17 1.17 .88 8 35 60 6 1.17 1.17 .88 11.875 70.6426533922479 120 6 1.17 1.17 .88 15.225457706434 95 180 6 1.17 1.17 .88 16 130 240 6 1.17 1.17 .88 16.6711784775435 170 300 6 1.17 1.17 .88 15 230 360 6 1.17 1.17 .88 12.9813561534016 300 420 6 1.17 1.17 .88 9.08352649928834 390 480 6 1.17 1.17 .88 6 440 540 6 1.17 1.17 .88 1 455 600 8 1.17 1.17 .88 Fuselage 16 16 0 0 0 #FALSE# #FALSE# #FALSE# 200 200 200 0 0 -250 10 1 1 .5 20 20 -187 4.69286637397673 1 1 .5 34.6982493428044 34 -147 3.40906959816482 1 1 .5 38.4939167780625 38 -123.763912970524 3.62957105748323 1 1 .5 41.1745623357011 40 -100 3.8550813803904 1 1 .5 50 50 50 0 1 1 .5 50 50 200 0 1 .49 .5 50 50 350 0 1.17 .01 .5 49.1745623357011 48.7609765646848 387.170703059455 0 1.12787320319928 .01 .5 47.9507696305896 43.7838648796625 457.644443201521 2.6279870136201 1.02 .27017071434839 .54954128440367 50.0829131987641 41.6271164828195 488.18306392975 3.76678138618881 1.42 .382911357232692 .571009174311927 69.4372745995465 36.4011492135461 562.180491078919 6.52616775048992 2.36 .502874631365385 .658390056229654 79.2129525693006 33.912593371035 597.417361149953 7.84016125729997 3.37 .56 .7 64.8914356033316 30.6774707757705 643.225292242296 10.7229151518541 3.16 .95528692879915 .68 27.6508753285978 30 650 12.3491246714022 .95 1 .5 0 0 800 35 1 1 .5 Rudder 16 105 240.441299848985 50.6359416074724 .1 .1 491.434084680351 193.964986856088 0 0 30 200 200 200 1 ElectroBox 30 15 25 0 77.1929824561403 10 5 0 0 #FALSE# ObjectList 2 "Fuselage 001" #TRUE# "Fuselage 002" #TRUE# Airfoil 16 1 0 .6 -.461538461538462 .3 -.5 .225 -.480769230769231 .15 -.461538461538462 .1 -.384615384615385 .05 -.307692307692308 0 -3.84615384615385E-02 0 3.84615384615385E-02 .05 .307692307692308 .1 .384615384615385 .15 .461538461538462 .2 .480769230769231 .3 .5 .6 .461538461538462 1 0 Airfoil 16 1 0 .6 -.461538461538462 .3 -.5 .225 -.480769230769231 .15 -.461538461538462 .1 -.384615384615385 .05 -.307692307692308 0 -3.84615384615385E-02 0 3.84615384615385E-02 .05 .307692307692308 .1 .384615384615385 .15 .461538461538462 .2 .480769230769231 .3 .5 .6 .461538461538462 1 0