# RCCAD File Format V 1.7.1 2 Wing Type 16 312.771197835923 804.392894264386 569.616365869791 .13 .13 -13.963639620999 68.4711329490693 50 -2.04398471489012 -.31843522630634 33 21 172 Wing Type 16 112.974300037499 569.616365869791 205.770791535643 .13 .13 54.5074933280702 121.539663948398 47.9560152851099 -9.21785036676756E-02 312.452762609617 33 21 172 Wing Type 16 387.23134531191 178.171968836943 83.3929468616158 .13 .13 492.318916457934 6.07053138384201 50 0 207.268995040178 33 21 172 2 Fuselage 11 16 0 0 0 #FALSE# #TRUE# #TRUE# 33 21 172 2 2 -75.4630854886012 43.1125278979039 1 1 .5 34.0277511086038 54.6510580819451 -67.6832213183779 28.6817801949312 1 1 .5 57.3582915761641 72.9519271813635 -56.2316751672867 18.9330899550547 1 1 .5 79.1026356796862 100 -30.8297592308844 9.91070890493145 1 1 .5 87.7583769012893 102.329590485502 .7823712513432 6.34081590918347 1 1 .5 126.601958311757 100.420174068102 61.8993898119703 -.572079265443701 1 1 .5 138.198424608916 95.562623993689 104.768745079497 -2.02164693796115 1 1 .5 137.74846249306 83.3264885872096 163.76276159218 -1.47268999019137 1 1 .5 126.747709993776 63.6747533669197 225.019980203792 -2.84544338220116 1 1 .5 89.2726358357148 36.0678836190843 261.622223848578 8.49085379278851 1 1 .5 25.5395884532619 7.14763856713205 271.273268995802 32.2110117643272 1 1 .5 Fuselage 6 16 368.448820431422 0 0 #FALSE# #TRUE# #TRUE# 33 21 172 2 2 -121.066132627005 46.4108512561371 1 1 .5 24.1920161155522 24 -117.73502119717 35.2064831291852 1 1 .5 38 38.828166899674 -109.27907703964 27.8054051651466 1 1 .5 45 45 -99.6762831663219 24.7645464841133 1 1 .5 45 45 200 24.8824433209929 1 1 .5 45 45 351.024126461411 25.026709356828 1 1 .5 Rudder 16 147.397630959364 151.511858641217 80 .1 .1 500 17.1938789410586 200.138725920326 0 62.4681382827394 33 21 172 1 ElectroBox 30 15 25 0 200 50 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