1 00:00:36,079 --> 00:00:37,910 radio-controlled model aircraft flying 2 00:00:37,910 --> 00:00:37,920 radio-controlled model aircraft flying 3 00:00:37,920 --> 00:00:40,470 radio-controlled model aircraft flying is one of america's most popular hobbies 4 00:00:40,470 --> 00:00:40,480 is one of america's most popular hobbies 5 00:00:40,480 --> 00:00:42,229 is one of america's most popular hobbies the people who fly these small-scale 6 00:00:42,229 --> 00:00:42,239 the people who fly these small-scale 7 00:00:42,239 --> 00:00:43,750 the people who fly these small-scale versions of their favorite planes have 8 00:00:43,750 --> 00:00:43,760 versions of their favorite planes have 9 00:00:43,760 --> 00:00:46,069 versions of their favorite planes have many reasons why they are interested 10 00:00:46,069 --> 00:00:46,079 many reasons why they are interested 11 00:00:46,079 --> 00:00:48,389 many reasons why they are interested some like the excitement of flying some 12 00:00:48,389 --> 00:00:48,399 some like the excitement of flying some 13 00:00:48,399 --> 00:00:49,430 some like the excitement of flying some like building them 14 00:00:49,430 --> 00:00:49,440 like building them 15 00:00:49,440 --> 00:00:55,830 like building them and some just enjoy the camaraderie 16 00:00:55,830 --> 00:00:55,840 17 00:00:55,840 --> 00:00:57,590 engineers at nasa's dryden flight 18 00:00:57,590 --> 00:00:57,600 engineers at nasa's dryden flight 19 00:00:57,600 --> 00:00:59,270 engineers at nasa's dryden flight research center in california 20 00:00:59,270 --> 00:00:59,280 research center in california 21 00:00:59,280 --> 00:01:01,029 research center in california use radio control aircraft for another 22 00:01:01,029 --> 00:01:01,039 use radio control aircraft for another 23 00:01:01,039 --> 00:01:03,670 use radio control aircraft for another reason research 24 00:01:03,670 --> 00:01:03,680 reason research 25 00:01:03,680 --> 00:01:05,109 reason research they know that meaningful data can be 26 00:01:05,109 --> 00:01:05,119 they know that meaningful data can be 27 00:01:05,119 --> 00:01:08,630 they know that meaningful data can be obtained from radio controlled aircraft 28 00:01:08,630 --> 00:01:08,640 obtained from radio controlled aircraft 29 00:01:08,640 --> 00:01:10,630 obtained from radio controlled aircraft they are using a 15 percent model of 30 00:01:10,630 --> 00:01:10,640 they are using a 15 percent model of 31 00:01:10,640 --> 00:01:11,990 they are using a 15 percent model of dry-in zone f-18 32 00:01:11,990 --> 00:01:12,000 dry-in zone f-18 33 00:01:12,000 --> 00:01:13,910 dry-in zone f-18 high alpha research vehicle that has 34 00:01:13,910 --> 00:01:13,920 high alpha research vehicle that has 35 00:01:13,920 --> 00:01:15,350 high alpha research vehicle that has been built as a proof-of-concept 36 00:01:15,350 --> 00:01:15,360 been built as a proof-of-concept 37 00:01:15,360 --> 00:01:19,830 been built as a proof-of-concept platform to conduct aerodynamic research 38 00:01:19,830 --> 00:01:19,840 39 00:01:19,840 --> 00:01:21,350 the model was made at dryden almost 40 00:01:21,350 --> 00:01:21,360 the model was made at dryden almost 41 00:01:21,360 --> 00:01:23,350 the model was made at dryden almost exclusively from standard rc model 42 00:01:23,350 --> 00:01:23,360 exclusively from standard rc model 43 00:01:23,360 --> 00:01:24,310 exclusively from standard rc model industry equipment 44 00:01:24,310 --> 00:01:24,320 industry equipment 45 00:01:24,320 --> 00:01:26,630 industry equipment like this aeron servo but a number of 46 00:01:26,630 --> 00:01:26,640 like this aeron servo but a number of 47 00:01:26,640 --> 00:01:28,469 like this aeron servo but a number of modifications had to be made in order to 48 00:01:28,469 --> 00:01:28,479 modifications had to be made in order to 49 00:01:28,479 --> 00:01:31,429 modifications had to be made in order to meet research specifications 50 00:01:31,429 --> 00:01:31,439 meet research specifications 51 00:01:31,439 --> 00:01:33,830 meet research specifications the fuselage made of fiberglass comes 52 00:01:33,830 --> 00:01:33,840 the fuselage made of fiberglass comes 53 00:01:33,840 --> 00:01:36,230 the fuselage made of fiberglass comes from an off-the-shelf model kit 54 00:01:36,230 --> 00:01:36,240 from an off-the-shelf model kit 55 00:01:36,240 --> 00:01:37,830 from an off-the-shelf model kit the wings and tail surfaces are made out 56 00:01:37,830 --> 00:01:37,840 the wings and tail surfaces are made out 57 00:01:37,840 --> 00:01:39,749 the wings and tail surfaces are made out of a styrofoam core and sheeted with 58 00:01:39,749 --> 00:01:39,759 of a styrofoam core and sheeted with 59 00:01:39,759 --> 00:01:42,469 of a styrofoam core and sheeted with balsa wood 60 00:01:42,469 --> 00:01:42,479 61 00:01:42,479 --> 00:01:44,469 entirely new engine inlets and exhaust 62 00:01:44,469 --> 00:01:44,479 entirely new engine inlets and exhaust 63 00:01:44,479 --> 00:01:45,910 entirely new engine inlets and exhaust stucks were made in order to more 64 00:01:45,910 --> 00:01:45,920 stucks were made in order to more 65 00:01:45,920 --> 00:01:47,109 stucks were made in order to more accurately represent 66 00:01:47,109 --> 00:01:47,119 accurately represent 67 00:01:47,119 --> 00:01:50,389 accurately represent the true f-18 inlet configuration 68 00:01:50,389 --> 00:01:50,399 the true f-18 inlet configuration 69 00:01:50,399 --> 00:01:52,830 the true f-18 inlet configuration this included functional boundary layer 70 00:01:52,830 --> 00:01:52,840 this included functional boundary layer 71 00:01:52,840 --> 00:01:54,149 this included functional boundary layer diverters 72 00:01:54,149 --> 00:01:54,159 diverters 73 00:01:54,159 --> 00:01:55,830 diverters stress carrying bulkheads made of a 74 00:01:55,830 --> 00:01:55,840 stress carrying bulkheads made of a 75 00:01:55,840 --> 00:01:57,990 stress carrying bulkheads made of a special laminate of end grain balsa wood 76 00:01:57,990 --> 00:01:58,000 special laminate of end grain balsa wood 77 00:01:58,000 --> 00:01:59,109 special laminate of end grain balsa wood and fiberglass 78 00:01:59,109 --> 00:01:59,119 and fiberglass 79 00:01:59,119 --> 00:02:00,469 and fiberglass had to be installed to handle the 80 00:02:00,469 --> 00:02:00,479 had to be installed to handle the 81 00:02:00,479 --> 00:02:01,910 had to be installed to handle the stresses encountered by the model in 82 00:02:01,910 --> 00:02:01,920 stresses encountered by the model in 83 00:02:01,920 --> 00:02:04,709 stresses encountered by the model in flight 84 00:02:04,709 --> 00:02:04,719 85 00:02:04,719 --> 00:02:06,709 some parts like the stabilator pivot 86 00:02:06,709 --> 00:02:06,719 some parts like the stabilator pivot 87 00:02:06,719 --> 00:02:08,790 some parts like the stabilator pivot mechanism were made by hand 88 00:02:08,790 --> 00:02:08,800 mechanism were made by hand 89 00:02:08,800 --> 00:02:10,309 mechanism were made by hand other types of material used were 90 00:02:10,309 --> 00:02:10,319 other types of material used were 91 00:02:10,319 --> 00:02:14,309 other types of material used were plywood carbon fiber and balsa wood 92 00:02:14,309 --> 00:02:14,319 plywood carbon fiber and balsa wood 93 00:02:14,319 --> 00:02:15,910 plywood carbon fiber and balsa wood the model's thrust comes from two 94 00:02:15,910 --> 00:02:15,920 the model's thrust comes from two 95 00:02:15,920 --> 00:02:17,830 the model's thrust comes from two commercially available ducted fan units 96 00:02:17,830 --> 00:02:17,840 commercially available ducted fan units 97 00:02:17,840 --> 00:02:19,270 commercially available ducted fan units that are 85 percent efficient in 98 00:02:19,270 --> 00:02:19,280 that are 85 percent efficient in 99 00:02:19,280 --> 00:02:21,589 that are 85 percent efficient in converting horsepower to thrust 100 00:02:21,589 --> 00:02:21,599 converting horsepower to thrust 101 00:02:21,599 --> 00:02:23,510 converting horsepower to thrust two model airplane engines power the fan 102 00:02:23,510 --> 00:02:23,520 two model airplane engines power the fan 103 00:02:23,520 --> 00:02:25,270 two model airplane engines power the fan units producing 11 pounds of static 104 00:02:25,270 --> 00:02:25,280 units producing 11 pounds of static 105 00:02:25,280 --> 00:02:28,790 units producing 11 pounds of static thrust each 106 00:02:28,790 --> 00:02:28,800 107 00:02:28,800 --> 00:02:30,390 the plane has been tracked on radar at 108 00:02:30,390 --> 00:02:30,400 the plane has been tracked on radar at 109 00:02:30,400 --> 00:02:32,550 the plane has been tracked on radar at 160 knots a speed which should be 110 00:02:32,550 --> 00:02:32,560 160 knots a speed which should be 111 00:02:32,560 --> 00:02:33,910 160 knots a speed which should be increased with the installation of 112 00:02:33,910 --> 00:02:33,920 increased with the installation of 113 00:02:33,920 --> 00:02:37,910 increased with the installation of liquid propane fuel mini turbo jets 114 00:02:37,910 --> 00:02:37,920 liquid propane fuel mini turbo jets 115 00:02:37,920 --> 00:02:39,430 liquid propane fuel mini turbo jets thrust vectoring vanes have been added 116 00:02:39,430 --> 00:02:39,440 thrust vectoring vanes have been added 117 00:02:39,440 --> 00:02:40,949 thrust vectoring vanes have been added to the model to make it true to the real 118 00:02:40,949 --> 00:02:40,959 to the model to make it true to the real 119 00:02:40,959 --> 00:02:43,270 to the model to make it true to the real aircraft but are not operational 120 00:02:43,270 --> 00:02:43,280 aircraft but are not operational 121 00:02:43,280 --> 00:02:45,030 aircraft but are not operational however an operational system has been 122 00:02:45,030 --> 00:02:45,040 however an operational system has been 123 00:02:45,040 --> 00:02:48,309 however an operational system has been designed for a future project 124 00:02:48,309 --> 00:02:48,319 designed for a future project 125 00:02:48,319 --> 00:02:49,910 designed for a future project the plane is fully instrumented to 126 00:02:49,910 --> 00:02:49,920 the plane is fully instrumented to 127 00:02:49,920 --> 00:02:52,470 the plane is fully instrumented to measure air speed angle of attack 128 00:02:52,470 --> 00:02:52,480 measure air speed angle of attack 129 00:02:52,480 --> 00:02:55,190 measure air speed angle of attack side slip and control surface positions 130 00:02:55,190 --> 00:02:55,200 side slip and control surface positions 131 00:02:55,200 --> 00:02:57,270 side slip and control surface positions three axis rate gyros measure the rate 132 00:02:57,270 --> 00:02:57,280 three axis rate gyros measure the rate 133 00:02:57,280 --> 00:02:58,149 three axis rate gyros measure the rate of rotation 134 00:02:58,149 --> 00:02:58,159 of rotation 135 00:02:58,159 --> 00:02:59,750 of rotation and three accelerometers measure the 136 00:02:59,750 --> 00:02:59,760 and three accelerometers measure the 137 00:02:59,760 --> 00:03:01,509 and three accelerometers measure the g-forces experienced by the model in 138 00:03:01,509 --> 00:03:01,519 g-forces experienced by the model in 139 00:03:01,519 --> 00:03:02,869 g-forces experienced by the model in flight 140 00:03:02,869 --> 00:03:02,879 flight 141 00:03:02,879 --> 00:03:04,710 flight it took six months to build at a cost of 142 00:03:04,710 --> 00:03:04,720 it took six months to build at a cost of 143 00:03:04,720 --> 00:03:06,229 it took six months to build at a cost of approximately twenty five thousand 144 00:03:06,229 --> 00:03:06,239 approximately twenty five thousand 145 00:03:06,239 --> 00:03:07,670 approximately twenty five thousand dollars 146 00:03:07,670 --> 00:03:07,680 dollars 147 00:03:07,680 --> 00:03:09,430 dollars these modifications make it truly 148 00:03:09,430 --> 00:03:09,440 these modifications make it truly 149 00:03:09,440 --> 00:03:11,350 these modifications make it truly capable performing as a flight research 150 00:03:11,350 --> 00:03:11,360 capable performing as a flight research 151 00:03:11,360 --> 00:03:11,990 capable performing as a flight research vehicle 152 00:03:11,990 --> 00:03:12,000 vehicle 153 00:03:12,000 --> 00:03:14,949 vehicle like its full-scale big brother rc 154 00:03:14,949 --> 00:03:14,959 like its full-scale big brother rc 155 00:03:14,959 --> 00:03:16,949 like its full-scale big brother rc subscale models like this have a unique 156 00:03:16,949 --> 00:03:16,959 subscale models like this have a unique 157 00:03:16,959 --> 00:03:18,470 subscale models like this have a unique quality that allows researchers to 158 00:03:18,470 --> 00:03:18,480 quality that allows researchers to 159 00:03:18,480 --> 00:03:20,070 quality that allows researchers to gather aerodynamic data 160 00:03:20,070 --> 00:03:20,080 gather aerodynamic data 161 00:03:20,080 --> 00:03:21,589 gather aerodynamic data which is difficult and expensive to 162 00:03:21,589 --> 00:03:21,599 which is difficult and expensive to 163 00:03:21,599 --> 00:03:23,350 which is difficult and expensive to obtain in wind tunnels 164 00:03:23,350 --> 00:03:23,360 obtain in wind tunnels 165 00:03:23,360 --> 00:03:24,949 obtain in wind tunnels models like this are especially suited 166 00:03:24,949 --> 00:03:24,959 models like this are especially suited 167 00:03:24,959 --> 00:03:26,710 models like this are especially suited for getting aerodynamic data 168 00:03:26,710 --> 00:03:26,720 for getting aerodynamic data 169 00:03:26,720 --> 00:03:28,710 for getting aerodynamic data like performing parameter identification 170 00:03:28,710 --> 00:03:28,720 like performing parameter identification 171 00:03:28,720 --> 00:03:30,869 like performing parameter identification studies and for confirming the basic 172 00:03:30,869 --> 00:03:30,879 studies and for confirming the basic 173 00:03:30,879 --> 00:03:31,990 studies and for confirming the basic airworthiness of unique 174 00:03:31,990 --> 00:03:32,000 airworthiness of unique 175 00:03:32,000 --> 00:03:34,710 airworthiness of unique aircraft configurations research and 176 00:03:34,710 --> 00:03:34,720 aircraft configurations research and 177 00:03:34,720 --> 00:03:36,470 aircraft configurations research and advanced control theory can also be done 178 00:03:36,470 --> 00:03:36,480 advanced control theory can also be done 179 00:03:36,480 --> 00:03:38,789 advanced control theory can also be done by using existing technology 180 00:03:38,789 --> 00:03:38,799 by using existing technology 181 00:03:38,799 --> 00:03:40,309 by using existing technology a flight control computer can be 182 00:03:40,309 --> 00:03:40,319 a flight control computer can be 183 00:03:40,319 --> 00:03:41,830 a flight control computer can be installed that would allow the aircraft 184 00:03:41,830 --> 00:03:41,840 installed that would allow the aircraft 185 00:03:41,840 --> 00:03:43,350 installed that would allow the aircraft to gather data at specific flight 186 00:03:43,350 --> 00:03:43,360 to gather data at specific flight 187 00:03:43,360 --> 00:03:45,430 to gather data at specific flight conditions 188 00:03:45,430 --> 00:03:45,440 conditions 189 00:03:45,440 --> 00:03:47,110 conditions radio-controlled model aircraft flying 190 00:03:47,110 --> 00:03:47,120 radio-controlled model aircraft flying 191 00:03:47,120 --> 00:03:49,350 radio-controlled model aircraft flying is a great hobby but for nasa's dryden 192 00:03:49,350 --> 00:03:49,360 is a great hobby but for nasa's dryden 193 00:03:49,360 --> 00:03:50,550 is a great hobby but for nasa's dryden flight research center 194 00:03:50,550 --> 00:03:50,560 flight research center 195 00:03:50,560 --> 00:03:52,229 flight research center they are just another innovative tool in 196 00:03:52,229 --> 00:03:52,239 they are just another innovative tool in 197 00:03:52,239 --> 00:03:58,830 they are just another innovative tool in advancing their frontiers of flight 198 00:03:58,830 --> 00:03:58,840 199 00:03:58,840 --> 00:04:08,550 research 200 00:04:08,550 --> 00:04:08,560 201 00:04:08,560 --> 00:04:10,640 you