1 00:01:14,320 --> 00:01:10,480 the thunder of powerful engines echoing 2 00:01:18,700 --> 00:01:14,330 in the desert air a plume of steam 3 00:01:24,640 --> 00:01:18,710 billowing towards the sky sparks flying 4 00:01:29,620 --> 00:01:24,650 from electrical wires the blast from a 5 00:01:31,420 --> 00:01:29,630 controlled explosion these sights and 6 00:01:33,580 --> 00:01:31,430 sounds belong to one of the world's 7 00:01:37,480 --> 00:01:33,590 finest state-of-the-art facilities for 8 00:01:39,100 --> 00:01:37,490 propulsion and materials testing in the 9 00:01:39,969 --> 00:01:39,110 desert northeast of Las Cruces New 10 00:01:42,760 --> 00:01:39,979 Mexico 11 00:01:44,680 --> 00:01:42,770 NASA's white sands test facility stands 12 00:01:46,780 --> 00:01:44,690 ready to challenge the safety and 13 00:02:03,370 --> 00:01:46,790 reliability of items slated for 14 00:02:12,229 --> 00:02:06,770 the goal at White Sands is to minimize 15 00:02:17,240 --> 00:02:12,239 flight risks safety no matter what is 16 00:02:21,740 --> 00:02:17,250 the first concern from rocket engines to 17 00:02:29,090 --> 00:02:21,750 film for a camera everything flown on a 18 00:02:33,390 --> 00:02:30,960 carefully controlled test parameters 19 00:02:38,180 --> 00:02:33,400 determine the strengths and weaknesses 20 00:02:44,880 --> 00:02:41,400 this testing is crucial to mission 21 00:02:48,000 --> 00:02:44,890 success taking the risk here on earth 22 00:02:50,340 --> 00:02:48,010 first will help avoid having to solve a 23 00:02:55,410 --> 00:02:50,350 problem miles away from home in the 24 00:02:57,720 --> 00:02:55,420 unforgiving space environment as part of 25 00:02:59,730 --> 00:02:57,730 NASA's Johnson Space Center the white 26 00:03:04,500 --> 00:02:59,740 sands test facility is primarily a 27 00:03:05,970 --> 00:03:04,510 support organization the testing 28 00:03:08,160 --> 00:03:05,980 requirements for the Johnson Space 29 00:03:12,750 --> 00:03:08,170 Center are the first priority for this 30 00:03:15,120 --> 00:03:12,760 facility however it also supports other 31 00:03:17,760 --> 00:03:15,130 NASA centers various government agencies 32 00:03:23,120 --> 00:03:17,770 and aerospace related commercial 33 00:03:27,810 --> 00:03:25,590 client provides the test article and 34 00:03:34,710 --> 00:03:27,820 defines the technical and schedule 35 00:03:36,960 --> 00:03:34,720 requirements white sands personnel 36 00:03:40,950 --> 00:03:36,970 develop and conduct the test program to 37 00:03:46,720 --> 00:03:43,900 NASA's white sands test facility employs 38 00:03:49,660 --> 00:03:46,730 a team of over 700 civil servants and 39 00:03:53,130 --> 00:03:49,670 contractors this self-sufficient 40 00:03:56,830 --> 00:03:53,140 facility includes an administrative area 41 00:04:02,410 --> 00:03:56,840 two propulsion test areas and a 42 00:04:05,530 --> 00:04:02,420 laboratories area the moderate weather 43 00:04:07,630 --> 00:04:05,540 arid climate and remote location make 44 00:04:12,090 --> 00:04:07,640 this an ideal site for propulsion and 45 00:04:14,470 --> 00:04:12,100 hazardous material testing built in 1964 46 00:04:16,990 --> 00:04:14,480 facilities here contest the entire 47 00:04:23,530 --> 00:04:17,000 propulsion system at one time to see how 48 00:04:25,510 --> 00:04:23,540 the components interact while the larger 49 00:04:27,130 --> 00:04:25,520 Saturn 5 engines which would push the 50 00:04:31,360 --> 00:04:27,140 Apollo spacecraft off the launch pad 51 00:04:33,040 --> 00:04:31,370 were tested at another NASA facility the 52 00:04:34,630 --> 00:04:33,050 white sands facility began its 53 00:04:36,880 --> 00:04:34,640 propulsion work with the development and 54 00:04:39,990 --> 00:04:36,890 certification testing of Apollo's 55 00:04:42,460 --> 00:04:40,000 service module and lunar module engines 56 00:04:51,159 --> 00:04:42,470 these engines were crucial to the 57 00:04:53,110 --> 00:04:51,169 success of the Apollo missions the 58 00:04:57,159 --> 00:04:53,120 service module engine put the astronauts 59 00:05:00,120 --> 00:04:57,169 into lunar orbit then the lunar module 60 00:05:02,860 --> 00:05:00,130 descent engine landed them on the moon 61 00:05:04,360 --> 00:05:02,870 the lunar module ascent engine blasted 62 00:05:08,830 --> 00:05:04,370 them off the moon and back into lunar 63 00:05:14,770 --> 00:05:08,840 orbit and the service module engine 64 00:05:16,840 --> 00:05:14,780 brought them back home four dozen tiny 65 00:05:18,820 --> 00:05:16,850 reaction control engines on the lunar 66 00:05:23,650 --> 00:05:18,830 module and command service module 67 00:05:25,570 --> 00:05:23,660 steered the vehicles through space over 68 00:05:27,670 --> 00:05:25,580 the years White Sands has tested more 69 00:05:32,240 --> 00:05:27,680 than three hundred engines in over two 70 00:05:41,010 --> 00:05:35,430 each test is conducted to make sure that 71 00:05:44,160 --> 00:05:41,020 the engines are safe and reliable in the 72 00:05:46,370 --> 00:05:44,170 early 1970s white sands began tests for 73 00:05:49,020 --> 00:05:46,380 the shuttles on-orbit propulsion systems 74 00:05:54,900 --> 00:05:49,030 including the orbital maneuvering system 75 00:05:57,150 --> 00:05:54,910 and the reaction control system three 76 00:05:58,680 --> 00:05:57,160 high fidelity flight light test articles 77 00:06:02,310 --> 00:05:58,690 were used for the development and 78 00:06:03,840 --> 00:06:02,320 qualification of these systems recently 79 00:06:07,710 --> 00:06:03,850 these test articles entered a new phase 80 00:06:09,510 --> 00:06:07,720 of testing in order to identify the life 81 00:06:11,700 --> 00:06:09,520 cycle limitations of the shuttle 82 00:06:18,210 --> 00:06:11,710 propulsion systems nASA has developed 83 00:06:19,710 --> 00:06:18,220 the fleet leader test program as part of 84 00:06:21,720 --> 00:06:19,720 this program white sands will 85 00:06:24,150 --> 00:06:21,730 periodically operate the test articles 86 00:06:28,020 --> 00:06:24,160 to see how repeated firings affect the 87 00:06:30,270 --> 00:06:28,030 system these test articles will undergo 88 00:06:35,040 --> 00:06:30,280 more firings and checkouts than any of 89 00:06:37,290 --> 00:06:35,050 the corresponding flight systems as a 90 00:06:39,659 --> 00:06:37,300 result shuttle component problems 91 00:06:41,210 --> 00:06:39,669 resulting from long-term exposure to 92 00:06:44,310 --> 00:06:41,220 corrosive rocket propellants and 93 00:06:50,270 --> 00:06:44,320 multi-mission operation can be resolved 94 00:06:56,060 --> 00:06:52,890 propulsion testing is conducted in two 95 00:07:02,340 --> 00:06:56,070 separate locations designated 300 and 96 00:07:05,340 --> 00:07:02,350 400 test areas in the 300 test area to 97 00:07:07,900 --> 00:07:05,350 test stands operate at normal or ambient 98 00:07:10,690 --> 00:07:07,910 atmospheric pressure 99 00:07:12,550 --> 00:07:10,700 these stands are hinged to accommodate 100 00:07:14,490 --> 00:07:12,560 rocket systems which must be tested in 101 00:07:17,380 --> 00:07:14,500 both horizontal and vertical 102 00:07:19,120 --> 00:07:17,390 orientations such as the steering 103 00:07:25,330 --> 00:07:19,130 thrusters which control the shuttles 104 00:07:26,950 --> 00:07:25,340 position in orbit a third test chamber 105 00:07:28,990 --> 00:07:26,960 allows rocket engine tests to be 106 00:07:34,390 --> 00:07:29,000 conducted under simulated space vacuum 107 00:07:37,900 --> 00:07:34,400 condition the largest of these tests and 108 00:07:40,330 --> 00:07:37,910 302 was extended to a height of 58 feet 109 00:07:45,220 --> 00:07:40,340 during the Viking Mars Lander program in 110 00:07:47,470 --> 00:07:45,230 the early 1970s at that time it was used 111 00:07:49,960 --> 00:07:47,480 to simulate the physical and biological 112 00:07:52,810 --> 00:07:49,970 effects of a rocket engine landing on 113 00:07:54,490 --> 00:07:52,820 Martian soil this work led to 114 00:07:56,800 --> 00:07:54,500 improvements to the rocket engine and 115 00:08:00,970 --> 00:07:56,810 its fuel prior to the launch of the 116 00:08:03,130 --> 00:08:00,980 Viking probe the stand has since been 117 00:08:08,740 --> 00:08:03,140 modified to accommodate vacuum testing 118 00:08:10,960 --> 00:08:08,750 of space station propulsion systems one 119 00:08:13,210 --> 00:08:10,970 of the largest instant steam generating 120 00:08:17,260 --> 00:08:13,220 systems in the country is located in the 121 00:08:19,210 --> 00:08:17,270 400 test area it can generate over 3/4 122 00:08:22,270 --> 00:08:19,220 of a million horsepower which would 123 00:08:27,499 --> 00:08:22,280 equal the power of over 5,000 automobile 124 00:08:32,579 --> 00:08:30,570 this steam generator closely simulates 125 00:08:34,589 --> 00:08:32,589 the space environment by allowing the 126 00:08:36,990 --> 00:08:34,599 interior of the altitude chambers to 127 00:08:44,040 --> 00:08:37,000 remain in a near vacuum during an engine 128 00:08:46,500 --> 00:08:44,050 firing to create the vacuum the engine 129 00:08:50,700 --> 00:08:46,510 fires into a large specially shaped duct 130 00:08:52,650 --> 00:08:50,710 which vents to the outside inside the 131 00:08:54,960 --> 00:08:52,660 duct our nozzles that inject cooling 132 00:08:56,670 --> 00:08:54,970 water and shoot high-pressure steam in 133 00:09:00,090 --> 00:08:56,680 the same direction as the exhaust is 134 00:09:03,030 --> 00:09:00,100 traveling the steam is accelerated to 135 00:09:05,730 --> 00:09:03,040 supersonic speeds as it is ejected by 136 00:09:07,980 --> 00:09:05,740 the system this creates a low pressure 137 00:09:10,530 --> 00:09:07,990 which has enough suction to pull all the 138 00:09:14,430 --> 00:09:10,540 atmosphere and the Rockets exhaust out 139 00:09:16,680 --> 00:09:14,440 of the info stand as a result the engine 140 00:09:20,850 --> 00:09:16,690 and exhaust plume are kept in a near 141 00:09:22,980 --> 00:09:20,860 vacuum testing under vacuum conditions 142 00:09:25,320 --> 00:09:22,990 is vital because rocket engines perform 143 00:09:28,530 --> 00:09:25,330 significantly better in space than in 144 00:09:30,300 --> 00:09:28,540 tests at atmospheric pressure this 145 00:09:35,519 --> 00:09:30,310 difference in performance must be 146 00:09:38,970 --> 00:09:35,529 measured precisely test stands for o1 147 00:09:42,079 --> 00:09:38,980 and 403 our altitude chambers used for 148 00:09:44,460 --> 00:09:42,089 testing liquid propellant engines a 149 00:09:47,070 --> 00:09:44,470 full-scale shuttle orbital maneuvering 150 00:09:49,650 --> 00:09:47,080 system pod and a flight type orbital 151 00:09:54,800 --> 00:09:49,660 maneuvering engine are installed in test 152 00:10:00,930 --> 00:09:57,660 another specialized vacuum test stand 153 00:10:02,520 --> 00:10:00,940 designated 405 was designed to determine 154 00:10:04,470 --> 00:10:02,530 the performance of the solid rocket 155 00:10:06,810 --> 00:10:04,480 motors typically used to boost 156 00:10:10,830 --> 00:10:06,820 spacecraft into orbits higher than the 157 00:10:12,780 --> 00:10:10,840 shuttle can reach solid rocket motor 158 00:10:15,630 --> 00:10:12,790 testing is difficult because these 159 00:10:19,470 --> 00:10:15,640 motors are often spun as they are fired 160 00:10:22,890 --> 00:10:19,480 a special fixture was set up to spin the 161 00:10:26,520 --> 00:10:22,900 motors at rates up to 125 revolutions 162 00:10:28,710 --> 00:10:26,530 per minute motor pressures temperatures 163 00:10:30,870 --> 00:10:28,720 and thrust outputs are measured to 164 00:10:34,710 --> 00:10:30,880 verify compliance with performance 165 00:10:37,020 --> 00:10:34,720 guidelines this stand can also test 166 00:10:43,320 --> 00:10:37,030 liquid fuel rocket engines such as the 167 00:10:44,520 --> 00:10:43,330 shuttles steering thrusters each test 168 00:10:48,140 --> 00:10:44,530 stand is operated from the 169 00:10:50,340 --> 00:10:48,150 blast-resistant control center 170 00:10:52,530 --> 00:10:50,350 underground tunnels connect the stands 171 00:11:03,050 --> 00:10:52,540 with the control center and protect the 172 00:11:07,740 --> 00:11:06,120 each test article is instrumented with 173 00:11:10,920 --> 00:11:07,750 hundreds of devices each measure 174 00:11:14,819 --> 00:11:10,930 pressures temperatures vibrations and 175 00:11:16,500 --> 00:11:14,829 flow rates the test procedure is 176 00:11:24,259 --> 00:11:16,510 precisely controlled to allow a 177 00:11:31,129 --> 00:11:27,120 for sets of computers acquire and 178 00:11:36,329 --> 00:11:33,930 these computers offer real-time test 179 00:11:41,790 --> 00:11:36,339 control plus digital and color graphic 180 00:11:43,800 --> 00:11:41,800 data displays engineers analyze the data 181 00:11:47,490 --> 00:11:43,810 to determine if the system met 182 00:11:48,990 --> 00:11:47,500 performance objectives following a 183 00:11:50,910 --> 00:11:49,000 firing the propulsion system is 184 00:11:56,850 --> 00:11:50,920 carefully checked out and examined for 185 00:12:00,120 --> 00:11:56,860 damage propulsion testing is more than 186 00:12:02,220 --> 00:12:00,130 just fire and smoke often white sands 187 00:12:04,079 --> 00:12:02,230 personnel must develop procedures were 188 00:12:07,319 --> 00:12:04,089 safely handling toxic or hazardous 189 00:12:10,550 --> 00:12:07,329 propellants in various situations such 190 00:12:12,990 --> 00:12:10,560 as loading propellants onto the shuttle 191 00:12:15,120 --> 00:12:13,000 other work involves continued 192 00:12:17,579 --> 00:12:15,130 development of environmentally safe 193 00:12:21,520 --> 00:12:17,589 systems or destroying toxic fuel waste 194 00:12:26,180 --> 00:12:23,840 techniques are also developed for 195 00:12:27,830 --> 00:12:26,190 cleaning and refurbishing shuttle 196 00:12:30,080 --> 00:12:27,840 propellant components which have 197 00:12:38,060 --> 00:12:30,090 accumulated contamination during more 198 00:12:40,100 --> 00:12:38,070 than 10 years of flight operations many 199 00:12:42,200 --> 00:12:40,110 special projects at white sands are 200 00:12:47,420 --> 00:12:42,210 supported by an extensive laboratory 201 00:12:50,090 --> 00:12:47,430 complex the laboratories area has nine 202 00:12:52,040 --> 00:12:50,100 remote tested cells designed for high 203 00:12:55,270 --> 00:12:52,050 pressure testing with gaseous and liquid 204 00:13:01,000 --> 00:12:58,520 there are also 14 remote test cells 205 00:13:03,350 --> 00:13:01,010 capable of withstanding explosions and 206 00:13:07,280 --> 00:13:03,360 designed for operation with hazardous 207 00:13:08,900 --> 00:13:07,290 toxic fluids in this area special 208 00:13:14,990 --> 00:13:08,910 equipment is used to examine the 209 00:13:16,700 --> 00:13:15,000 ignition combustion and explosive 210 00:13:21,140 --> 00:13:16,710 properties of typical spacecraft 211 00:13:23,120 --> 00:13:21,150 materials and propellers white sands has 212 00:13:26,390 --> 00:13:23,130 one of the most extensive materials 213 00:13:29,360 --> 00:13:26,400 testing laboratories in the world this 214 00:13:32,140 --> 00:13:29,370 lab characterizes materials on earth so 215 00:13:35,180 --> 00:13:32,150 that they can be depended on in space 216 00:13:37,850 --> 00:13:35,190 over 90% of all the nonmetallic 217 00:13:40,610 --> 00:13:37,860 materials flown during the Apollo Skylab 218 00:13:44,480 --> 00:13:40,620 and shuttle programs have been tested at 219 00:13:46,280 --> 00:13:44,490 white sands currently work focuses on 220 00:13:50,530 --> 00:13:46,290 materials proposed for use on the 221 00:13:53,480 --> 00:13:50,540 shuttle its payloads and space station 222 00:13:57,470 --> 00:13:53,490 among the unique tests conducted here is 223 00:13:59,240 --> 00:13:57,480 the flammability of metals white sands 224 00:14:07,820 --> 00:13:59,250 is a proven leader in this type of 225 00:14:11,870 --> 00:14:10,190 recently hypervelocity particle 226 00:14:25,160 --> 00:14:11,880 launchers have been added to white sands 227 00:14:26,990 --> 00:14:25,170 arsenal of tools these light gas guns 228 00:14:29,600 --> 00:14:27,000 propel objects up to one inch in 229 00:14:33,199 --> 00:14:29,610 diameter at speeds of nearly seven 230 00:14:36,590 --> 00:14:33,209 kilometers per second or ten times as 231 00:14:39,079 --> 00:14:36,600 fast as a high-powered rifle this 232 00:14:43,009 --> 00:14:39,089 simulates the impact of meteoroids and 233 00:14:47,000 --> 00:14:43,019 orbital debris on hazardous targets such 234 00:14:52,630 --> 00:14:47,010 as pressurized containers propellant 235 00:14:59,920 --> 00:14:55,400 there is more to the lab area than 236 00:15:02,360 --> 00:14:59,930 testing materials or studying explosions 237 00:15:05,449 --> 00:15:02,370 often parts that have failed on board 238 00:15:06,860 --> 00:15:05,459 the shuttle are analyzed in the 239 00:15:10,819 --> 00:15:06,870 controlled environment of the lab 240 00:15:12,650 --> 00:15:10,829 engineers try to mimic the failures from 241 00:15:17,930 --> 00:15:12,660 that they can identify the specific 242 00:15:20,210 --> 00:15:17,940 problem and work on a solution an other 243 00:15:23,120 --> 00:15:20,220 area of interest is payloads outgassing 244 00:15:27,170 --> 00:15:23,130 or the migration of molecules out of 245 00:15:31,460 --> 00:15:27,180 organic products tests are conducted on 246 00:15:35,540 --> 00:15:31,470 everything from laptop computers to 247 00:15:38,480 --> 00:15:35,550 animal enclosures to film for onboard 248 00:15:40,250 --> 00:15:38,490 cameras to ensure that nothing toxic is 249 00:15:44,120 --> 00:15:40,260 released from materials due to 250 00:15:46,370 --> 00:15:44,130 outgassing also payloads that fly 251 00:15:48,410 --> 00:15:46,380 together are tested to make sure that 252 00:15:52,790 --> 00:15:48,420 one payloads outgassing does not 253 00:15:54,769 --> 00:15:52,800 contaminate other payloads and white 254 00:15:57,889 --> 00:15:54,779 sands clean rooms are used continuously 255 00:15:59,510 --> 00:15:57,899 to precision clean all the parts used in 256 00:16:03,800 --> 00:15:59,520 rocket propellant and liquid oxygen 257 00:16:07,040 --> 00:16:03,810 tests these clean rooms are an integral 258 00:16:08,900 --> 00:16:07,050 part of the test program tests using 259 00:16:12,620 --> 00:16:08,910 rocket fuels cannot be conducted without 260 00:16:14,840 --> 00:16:12,630 precision clean parts if a small bit of 261 00:16:17,870 --> 00:16:14,850 organic material is on the test article 262 00:16:19,360 --> 00:16:17,880 and it is tested in pure oxygen a fire 263 00:16:21,280 --> 00:16:19,370 could result 264 00:16:23,950 --> 00:16:21,290 the clean room not only ensures 265 00:16:26,620 --> 00:16:23,960 uncontaminated test results but more 266 00:16:35,410 --> 00:16:26,630 importantly provides a necessary safety 267 00:16:38,170 --> 00:16:35,420 factor one indispensable and rather 268 00:16:42,640 --> 00:16:38,180 unusual test capability is the odor 269 00:16:45,310 --> 00:16:42,650 panel since 1967 a panel of volunteers 270 00:16:47,800 --> 00:16:45,320 has sniffed literally every item that 271 00:16:51,520 --> 00:16:47,810 has flown in the crew cabins of NASA's 272 00:16:53,290 --> 00:16:51,530 manned spacecraft this is important 273 00:17:09,600 --> 00:16:53,300 because a bad odor permeating an 274 00:17:24,770 --> 00:17:16,390 and alysus calibration valve disassembly 275 00:17:34,910 --> 00:17:30,730 x-ray special component-level testing 276 00:17:39,770 --> 00:17:34,920 and photography for all propulsion and 277 00:17:41,660 --> 00:17:39,780 laboratory activities technical support 278 00:17:45,470 --> 00:17:41,670 at white sands doesn't stop with the 279 00:17:47,450 --> 00:17:45,480 completion of the test these engineers 280 00:17:49,220 --> 00:17:47,460 scientists and technicians are 281 00:17:53,330 --> 00:17:49,230 determined to provide the answers to 282 00:17:55,370 --> 00:17:53,340 whatever questions might be posed they 283 00:17:58,520 --> 00:17:55,380 have even compiled several handbooks on 284 00:17:59,750 --> 00:17:58,530 aerospace fluid hazards as well as 285 00:18:07,310 --> 00:17:59,760 provided support for special 286 00:18:09,500 --> 00:18:07,320 investigations and hazard assessments in 287 00:18:11,960 --> 00:18:09,510 addition to providing top-notch test 288 00:18:13,850 --> 00:18:11,970 cells and laboratories the white sands 289 00:18:22,270 --> 00:18:13,860 test facility also supports another 290 00:18:27,650 --> 00:18:25,220 dry gypsum lake bed at the nearby US 291 00:18:30,530 --> 00:18:27,660 Army White Sands Missile Range provides 292 00:18:32,600 --> 00:18:30,540 two seven mile long runways for shuttle 293 00:18:36,740 --> 00:18:32,610 landing operations and astronaut 294 00:18:39,170 --> 00:18:36,750 training designated white sands Space 295 00:18:41,810 --> 00:18:39,180 Harbor this area of the Missile Range 296 00:18:52,310 --> 00:18:41,820 serves as an alternate landing site for 297 00:18:57,230 --> 00:18:54,710 although only one shuttle has landed 298 00:18:59,990 --> 00:18:57,240 here the Space Harbor is used everyday 299 00:19:03,230 --> 00:19:00,000 and often at night as an essential 300 00:19:05,180 --> 00:19:03,240 training ground for shuttle pilots here 301 00:19:06,620 --> 00:19:05,190 astronauts practice approaches and 302 00:19:08,899 --> 00:19:06,630 landings using the shuttle training 303 00:19:10,360 --> 00:19:08,909 aircraft which mimics the shuttles 304 00:19:18,350 --> 00:19:10,370 flight characteristics and 305 00:19:20,480 --> 00:19:18,360 instrumentation in 1989 a third runway 306 00:19:23,389 --> 00:19:20,490 was added to Train astronauts for 307 00:19:26,419 --> 00:19:23,399 transatlantic abort landings this 308 00:19:28,340 --> 00:19:26,429 shorter and narrower runway is almost an 309 00:19:35,710 --> 00:19:28,350 exact duplicate in size and appearance 310 00:19:39,950 --> 00:19:37,759 located near the white sands test 311 00:19:41,659 --> 00:19:39,960 facility is another installation which 312 00:19:44,450 --> 00:19:41,669 provides an important service to the 313 00:19:47,680 --> 00:19:44,460 shuttle program the tracking and data 314 00:19:50,419 --> 00:19:47,690 relay satellite system ground terminals 315 00:19:53,119 --> 00:19:50,429 two terminals are located about four 316 00:19:56,240 --> 00:19:53,129 miles apart each is responsible for 317 00:19:59,060 --> 00:19:56,250 receiving voice television and data from 318 00:20:00,710 --> 00:19:59,070 orbiting shuttles both terminals are 319 00:20:03,470 --> 00:20:00,720 supervised by nasa's goddard space 320 00:20:13,780 --> 00:20:03,480 flight center and are not related to the 321 00:20:19,060 --> 00:20:15,910 the outstanding track record at white 322 00:20:21,520 --> 00:20:19,070 sands centers around its people they are 323 00:20:24,160 --> 00:20:21,530 involved in all facets of the test from 324 00:20:25,830 --> 00:20:24,170 inception to completion these 325 00:20:28,630 --> 00:20:25,840 professionals have the resources 326 00:20:30,790 --> 00:20:28,640 training and experience necessary to 327 00:20:33,910 --> 00:20:30,800 provide state-of-the-art support for 328 00:20:35,770 --> 00:20:33,920 various test requirements the future 329 00:20:40,510 --> 00:20:35,780 holds many challenges for the white 330 00:20:42,460 --> 00:20:40,520 sands test facility at white sands years 331 00:20:44,770 --> 00:20:42,470 of experience combined with the physical 332 00:20:46,900 --> 00:20:44,780 assets of the facility will continue to 333 00:20:49,240 --> 00:20:46,910 provide the capability to safely 334 00:20:53,950 --> 00:20:49,250 evaluate potential hazards which may 335 00:20:57,450 --> 00:20:53,960 arise on earth and in space whether it 336 00:21:01,750 --> 00:20:57,460 involves firing rocket engines 337 00:21:06,250 --> 00:21:01,760 evaluating advanced materials studying 338 00:21:11,080 --> 00:21:06,260 explosions or testing new exotic 339 00:21:13,600 --> 00:21:11,090 propellants today's work at the white 340 00:21:15,970 --> 00:21:13,610 sands test facility will continue to