1 00:00:26,990 --> 00:00:25,130 Ames Research Center has played and will 2 00:00:29,600 --> 00:00:27,000 continue to play an important role in 3 00:00:31,370 --> 00:00:29,610 returning the space shuttle flight games 4 00:00:33,740 --> 00:00:31,380 has contributed to safety of the shuttle 5 00:00:36,200 --> 00:00:33,750 in several ways computing simulations 6 00:00:38,210 --> 00:00:36,210 and lab tests generated new data for 7 00:00:39,770 --> 00:00:38,220 preparing the shuttle and new facilities 8 00:00:43,460 --> 00:00:39,780 here will provide operational support 9 00:00:45,530 --> 00:00:43,470 during missions during every launch a 10 00:00:48,049 --> 00:00:45,540 certain amount of debris falls away in 11 00:00:49,400 --> 00:00:48,059 order to understand this phenomena we 12 00:00:52,189 --> 00:00:49,410 needed to simulate the event without 13 00:00:54,350 --> 00:00:52,199 actually flying a shuttle a technique 14 00:00:56,899 --> 00:00:54,360 called computational fluid dynamics or 15 00:00:58,910 --> 00:00:56,909 cfd is a method of using computers to 16 00:01:01,310 --> 00:00:58,920 simulate airflow over the shuttle wing 17 00:01:03,410 --> 00:01:01,320 during launch and reentry it requires 18 00:01:07,240 --> 00:01:03,420 millions of calculations but it can 19 00:01:11,810 --> 00:01:09,800 we've been working very closely with a 20 00:01:14,090 --> 00:01:11,820 number of engineers at Johnson for a 21 00:01:16,010 --> 00:01:14,100 quite a number of years in developing 22 00:01:17,840 --> 00:01:16,020 our computational fluid dynamics tools 23 00:01:21,380 --> 00:01:17,850 we've helped supply them with 24 00:01:24,830 --> 00:01:21,390 computational capability to analyze the 25 00:01:27,109 --> 00:01:24,840 sense of the redesigned external tank as 26 00:01:28,999 --> 00:01:27,119 well as to understand the debris 27 00:01:30,590 --> 00:01:29,009 environment that the vehicle has to go 28 00:01:34,850 --> 00:01:30,600 through as it's flying through the air 29 00:01:37,279 --> 00:01:34,860 even very small pieces of debris when 30 00:01:40,309 --> 00:01:37,289 they're traveling extremely fast and 31 00:01:42,620 --> 00:01:40,319 still in part significant impact to the 32 00:01:44,419 --> 00:01:42,630 vehicle and these are things that we 33 00:01:46,490 --> 00:01:44,429 have to look out for that we're still at 34 00:01:48,080 --> 00:01:46,500 risk for but that we have a very good 35 00:01:52,010 --> 00:01:48,090 understanding of what that risk is and 36 00:01:53,690 --> 00:01:52,020 we can try to avoid it the super 37 00:01:56,210 --> 00:01:53,700 computing facility here at Ames is 38 00:01:57,620 --> 00:01:56,220 absolutely unique and it's the fastest 39 00:02:01,010 --> 00:01:57,630 operational supercomputer in the world 40 00:02:03,949 --> 00:02:01,020 and its really allowed us to analyze our 41 00:02:05,719 --> 00:02:03,959 data compute our cases and just do 42 00:02:08,059 --> 00:02:05,729 things that we never would have been 43 00:02:10,009 --> 00:02:08,069 able to do without this facility in 44 00:02:12,020 --> 00:02:10,019 addition to the Columbia supercomputer 45 00:02:14,090 --> 00:02:12,030 Ames has several test facilities that 46 00:02:17,180 --> 00:02:14,100 are necessary to validate the cfd 47 00:02:19,330 --> 00:02:17,190 simulations with real-world data one is 48 00:02:21,850 --> 00:02:19,340 the ballistic range 49 00:02:23,800 --> 00:02:21,860 the CFD folks thought they are 50 00:02:25,750 --> 00:02:23,810 constructed a pretty good code it will 51 00:02:28,330 --> 00:02:25,760 really predict the motion of the shuttle 52 00:02:30,220 --> 00:02:28,340 form fragments but they wanted to check 53 00:02:33,009 --> 00:02:30,230 it so they said look you guys in the 54 00:02:35,290 --> 00:02:33,019 range you fire maybe 2025 projectiles 55 00:02:38,160 --> 00:02:35,300 see how they actually fly and we'll see 56 00:02:41,170 --> 00:02:38,170 if we can predict them with the CFD code 57 00:02:44,080 --> 00:02:41,180 what we're firing is a small disk like 58 00:02:46,210 --> 00:02:44,090 projectile it's about 1.4 inches in 59 00:02:48,430 --> 00:02:46,220 diameter for these particular tests were 60 00:02:51,039 --> 00:02:48,440 firing at about Mach 3 or about one 61 00:02:53,589 --> 00:02:51,049 kilometer or a second another way of 62 00:02:55,420 --> 00:02:53,599 validating CFD results involve building 63 00:02:57,640 --> 00:02:55,430 a small model of the shuttle three 64 00:02:59,380 --> 00:02:57,650 percent of its actual size and equipping 65 00:03:01,420 --> 00:02:59,390 it with hundreds of miniature sensors 66 00:03:03,490 --> 00:03:01,430 this allowed us to look at design 67 00:03:05,350 --> 00:03:03,500 modifications on the fuel tanks fairings 68 00:03:08,250 --> 00:03:05,360 and other areas of shuttle that might 69 00:03:12,460 --> 00:03:10,960 we were looking at doing some fairly 70 00:03:14,830 --> 00:03:12,470 detailed measurements on a three percent 71 00:03:16,540 --> 00:03:14,840 scale model of the shuttle in its ascent 72 00:03:19,390 --> 00:03:16,550 configuration with the external tank and 73 00:03:21,160 --> 00:03:19,400 SRB is attached tests in the 70s were 74 00:03:22,090 --> 00:03:21,170 done as part of the design process they 75 00:03:23,740 --> 00:03:22,100 really didn't understand the 76 00:03:26,140 --> 00:03:23,750 aerodynamics of the vehicle until they 77 00:03:28,840 --> 00:03:26,150 did the wind tunnel tests and those 78 00:03:31,570 --> 00:03:28,850 tests were primarily concerned with the 79 00:03:33,370 --> 00:03:31,580 performance some loads measurements but 80 00:03:35,350 --> 00:03:33,380 certainly not the detail that we need to 81 00:03:36,580 --> 00:03:35,360 look at now to make sure that the 82 00:03:38,860 --> 00:03:36,590 vehicle is safe to fly and the 83 00:03:40,600 --> 00:03:38,870 modifications that are being made will 84 00:03:42,820 --> 00:03:40,610 be safe there's new measurement 85 00:03:46,570 --> 00:03:42,830 techniques in particular pressure 86 00:03:48,640 --> 00:03:46,580 sensitive paint gives a complete map of 87 00:03:51,010 --> 00:03:48,650 the pressure over the entire geometry 88 00:03:52,750 --> 00:03:51,020 new types of measurements using optical 89 00:03:54,580 --> 00:03:52,760 techniques have made measurements 90 00:03:56,590 --> 00:03:54,590 possible that we couldn't do back in the 91 00:03:58,270 --> 00:03:56,600 70s so it it really is much richer 92 00:04:00,130 --> 00:03:58,280 database now that we're able to generate 93 00:04:02,190 --> 00:04:00,140 for the for the shuttle those 94 00:04:04,350 --> 00:04:02,200 measurements helped validate our 95 00:04:07,090 --> 00:04:04,360 calculations and show that the 96 00:04:11,330 --> 00:04:07,100 computational work matches the real 97 00:04:15,140 --> 00:04:13,610 the agency had to develop a few repair 98 00:04:17,750 --> 00:04:15,150 materials and techniques for treating 99 00:04:19,550 --> 00:04:17,760 damage to the shuttles wings one of the 100 00:04:22,790 --> 00:04:19,560 critical test facilities at Ames is 101 00:04:24,620 --> 00:04:22,800 called an arc jet this is a closed wind 102 00:04:26,000 --> 00:04:24,630 tunnel that generates air speeds and 103 00:04:28,610 --> 00:04:26,010 heating similar to what the shuttle 104 00:04:30,439 --> 00:04:28,620 encounters during reentry the agency was 105 00:04:31,909 --> 00:04:30,449 concerned that a debris strike would 106 00:04:34,159 --> 00:04:31,919 punch a hole in the wing leading edge 107 00:04:36,590 --> 00:04:34,169 and so they came up with a concept of a 108 00:04:38,960 --> 00:04:36,600 plug this is a typical plug 109 00:04:41,000 --> 00:04:38,970 configuration it's designed with some 110 00:04:43,400 --> 00:04:41,010 curvature to fit over the curvature of 111 00:04:45,080 --> 00:04:43,410 the wing leading edge early in the test 112 00:04:47,150 --> 00:04:45,090 program a lot of the plugs were failing 113 00:04:49,219 --> 00:04:47,160 and we learn lessons from those failures 114 00:04:51,950 --> 00:04:49,229 we knew we had to change the materials 115 00:04:55,850 --> 00:04:51,960 we had to change the shape and the 116 00:04:57,440 --> 00:04:55,860 angles to really try to adjust this plug 117 00:05:00,200 --> 00:04:57,450 so that it will stands the entry 118 00:05:02,420 --> 00:05:00,210 conditions this data was passed on to 119 00:05:04,190 --> 00:05:02,430 another group of CFD engineers who 120 00:05:06,200 --> 00:05:04,200 focused on analyzing the effects of 121 00:05:08,270 --> 00:05:06,210 atmospheric heating on specific types of 122 00:05:11,960 --> 00:05:08,280 tile damage and the repairs that might 123 00:05:14,480 --> 00:05:11,970 be made to them one is the analysis of 124 00:05:17,420 --> 00:05:14,490 damage and the other is the analysis of 125 00:05:20,029 --> 00:05:17,430 repair the object of CFD is to analyze 126 00:05:23,000 --> 00:05:20,039 both and determine whether both are in 127 00:05:25,310 --> 00:05:23,010 fact good candidates for entry or not 128 00:05:28,879 --> 00:05:25,320 you need on the order of a hundred 129 00:05:31,640 --> 00:05:28,889 solutions in under 24 hours in order to 130 00:05:34,129 --> 00:05:31,650 put enough credible data on the table to 131 00:05:36,350 --> 00:05:34,139 make a decision we had the ability to do 132 00:05:38,810 --> 00:05:36,360 CFD but it took us three weeks to 133 00:05:41,029 --> 00:05:38,820 generate even one solution during the 134 00:05:42,500 --> 00:05:41,039 return flight program we've moved the 135 00:05:44,839 --> 00:05:42,510 capabilities to the Columbia 136 00:05:49,800 --> 00:05:44,849 supercomputer we can now turn around a 137 00:05:53,700 --> 00:05:51,780 after every landing it's extremely 138 00:05:56,010 --> 00:05:53,710 important to closely examine all the 139 00:05:57,750 --> 00:05:56,020 shuttle services for damage in the past 140 00:06:00,690 --> 00:05:57,760 this has been extremely tedious and a 141 00:06:02,100 --> 00:06:00,700 time-consuming chore done manually one 142 00:06:03,960 --> 00:06:02,110 of our research has developed a device 143 00:06:06,360 --> 00:06:03,970 that could speed up the task and create 144 00:06:08,310 --> 00:06:06,370 a much higher degree of accuracy we 145 00:06:11,370 --> 00:06:08,320 developed a handheld laser scanning 146 00:06:12,570 --> 00:06:11,380 device that helps the technicians it 147 00:06:14,640 --> 00:06:12,580 speeds up their measurements 148 00:06:16,230 --> 00:06:14,650 tremendously and it makes the 149 00:06:19,890 --> 00:06:16,240 measurements more accurate and more 150 00:06:21,810 --> 00:06:19,900 reliable so you put the unit over the 151 00:06:24,570 --> 00:06:21,820 tile and you press a button and it takes 152 00:06:26,100 --> 00:06:24,580 a scan in about two seconds they will 153 00:06:28,800 --> 00:06:26,110 know as soon as they take the 154 00:06:31,469 --> 00:06:28,810 measurement if there is a problem with 155 00:06:33,960 --> 00:06:31,479 that tile that needs to be repaired so 156 00:06:35,879 --> 00:06:33,970 it takes a lot of the human tedious work 157 00:06:37,920 --> 00:06:35,889 out of it and therefore I think it 158 00:06:43,020 --> 00:06:37,930 increases the safety because it 159 00:06:47,559 --> 00:06:45,490 some of the ongoing support the names is 160 00:06:51,800 --> 00:06:47,569 given to the space program has been 161 00:06:56,030 --> 00:06:53,600 the vertical motion simulator is 162 00:06:57,620 --> 00:06:56,040 actually a simulation of the space 163 00:07:00,620 --> 00:06:57,630 shuttle coming in through landing and 164 00:07:03,470 --> 00:07:00,630 roll out the simulator out here at NASA 165 00:07:05,690 --> 00:07:03,480 Ames Research Center is a fantastic 166 00:07:07,190 --> 00:07:05,700 simulator for us to not just practice 167 00:07:09,590 --> 00:07:07,200 normal landings but to also practice 168 00:07:11,030 --> 00:07:09,600 emergency landings any type of failure 169 00:07:13,640 --> 00:07:11,040 that could possibly happen to the Space 170 00:07:17,020 --> 00:07:13,650 Shuttle on touchdown things like blown 171 00:07:19,670 --> 00:07:17,030 tires or you know brakes not working 172 00:07:22,340 --> 00:07:19,680 nose wheel steering a nice kid hi 173 00:07:24,710 --> 00:07:22,350 crosswinds it's a high fidelity sim and 174 00:07:27,080 --> 00:07:24,720 Glenn tastic training another great 175 00:07:28,310 --> 00:07:27,090 thing about the sim is in the visuals it 176 00:07:29,719 --> 00:07:28,320 could put runways from all over the 177 00:07:31,790 --> 00:07:29,729 world so we train all of our backup 178 00:07:33,620 --> 00:07:31,800 landing sites we have two runways in 179 00:07:35,240 --> 00:07:33,630 Spain and one of France we can also land 180 00:07:38,840 --> 00:07:35,250 at Edwards Air Force Base in Southern 181 00:07:40,430 --> 00:07:38,850 California white sands and New Mexico we 182 00:07:41,659 --> 00:07:40,440 don't really have the resources to take 183 00:07:43,640 --> 00:07:41,669 an airplane out there and look at all 184 00:07:44,719 --> 00:07:43,650 those airfields so it's really efficient 185 00:07:48,609 --> 00:07:44,729 for us to come out here and see in the 186 00:07:54,319 --> 00:07:52,059 they're very few off-the-shelf solutions 187 00:07:56,929 --> 00:07:54,329 really comes down to building space 188 00:07:58,489 --> 00:07:56,939 flight hardware you need to use a lot of 189 00:08:00,489 --> 00:07:58,499 different disciplines and you need 190 00:08:03,019 --> 00:08:00,499 insights from a lot of different people 191 00:08:05,689 --> 00:08:03,029 I think we've been invaluable to the 192 00:08:07,699 --> 00:08:05,699 program as a center and so it's been 193 00:08:11,479 --> 00:08:07,709 very gratifying to help help the program 194 00:08:14,749 --> 00:08:11,489 move forward NASA Ames is committed to 195 00:08:17,419 --> 00:08:14,759 astronaut safety and mission success all 196 00:08:19,549 --> 00:08:17,429 of these contributions add up to 197 00:08:21,949 --> 00:08:19,559 something we're very proud of returning