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These are the user uploaded subtitles that are being translated: 1 00:00:04,000 --> 00:00:07,599 Our seafaring nature has translated well to the space age, 2 00:00:07,679 --> 00:00:11,959 sailing out into the unknown in search of riches of one kind or another. 3 00:00:12,998 --> 00:00:16,678 While Europe and Asia continue their interest in the resource-rich Moon, 4 00:00:16,758 --> 00:00:20,077 the United States and NASA have set their sights on nothing less 5 00:00:20,157 --> 00:00:22,357 than manned missions to Mars. 6 00:00:24,157 --> 00:00:26,156 Can they manage to go shore to shore 7 00:00:26,236 --> 00:00:29,876 on the most dangerous of unknown seas, deep space? 8 00:01:08,389 --> 00:01:12,628 With low Earth orbit harnessed, it is time to look further afield. 9 00:01:12,708 --> 00:01:15,348 To build a spacecraft and rocket system to reach Mars 10 00:01:15,428 --> 00:01:16,947 is a mammoth undertaking, 11 00:01:17,027 --> 00:01:19,627 but if successful, it will return the United States to the top of the space achievement ladder. 12 00:01:23,426 --> 00:01:24,786 The first requirement: 13 00:01:24,866 --> 00:01:28,825 a space capsule able to carry six astronauts for a long period of time 14 00:01:28,905 --> 00:01:31,145 and return them safely to Earth. 15 00:01:31,425 --> 00:01:35,784 Orion is its name and it has flown once already in a shakedown. 16 00:01:36,104 --> 00:01:39,823 The next flight will be an unmanned test mission past the moon, 17 00:01:39,903 --> 00:01:42,703 followed by a third manned mission. 18 00:01:45,183 --> 00:01:48,102 The components for the vehicle are developed around the country, 19 00:01:48,182 --> 00:01:51,461 tested and checked, then passed on for assembly. 20 00:01:51,541 --> 00:01:55,141 The minutest bolt and circuit is designed, tested, redesigned 21 00:01:55,221 --> 00:01:56,421 and tested again. 22 00:01:57,140 --> 00:01:58,860 Slowly the systems come together, 23 00:01:58,940 --> 00:02:01,620 with the aid of some breakthrough technology, 24 00:02:01,700 --> 00:02:05,939 particularly in manufacturing methods, new materials and processes. 25 00:02:06,539 --> 00:02:09,258 The first thing to notice is that NASA have gone back 26 00:02:09,338 --> 00:02:13,858 to the classic conic shape like Apollo, the safest design yet devised. 27 00:02:14,338 --> 00:02:18,897 Avionics, control systems, computer software and a glass cockpit, 28 00:02:18,977 --> 00:02:20,976 all state of the art. 29 00:02:25,136 --> 00:02:28,055 ...and the concept was to go with a glass cockpit 30 00:02:28,135 --> 00:02:32,134 and what that means is that the instruments are all images 31 00:02:32,214 --> 00:02:33,174 on a computer screen. 32 00:02:33,254 --> 00:02:37,693 They are all on glass, so rather than flipping a physical switch, 33 00:02:37,773 --> 00:02:41,613 the crew brings up a computer screen and flips a virtual switch, 34 00:02:41,693 --> 00:02:44,532 a little icon of a switch or icon of a valve, 35 00:02:44,612 --> 00:02:49,611 and with the exception of seven panels right around the computer screens, 36 00:02:49,691 --> 00:02:51,691 which have about 60 switches, 37 00:02:51,771 --> 00:02:56,050 that is all of the cockpit of Orion happens on the glass. 38 00:02:56,130 --> 00:02:57,970 One big benefit is the weight savings 39 00:02:58,050 --> 00:03:00,330 because you don't have to have a physical switch. 40 00:03:00,410 --> 00:03:01,809 And having a physical switch, 41 00:03:01,889 --> 00:03:04,089 not only is there the weight of the switch, 42 00:03:04,169 --> 00:03:07,168 but you also have the weight of the wire to the switch, 43 00:03:07,248 --> 00:03:10,808 and you have to have the weight of circuitry that takes that wire 44 00:03:10,888 --> 00:03:13,647 and feeds it into the vehicle computers. 45 00:03:15,367 --> 00:03:18,286 Because of Orion's size, its all-important heat shield 46 00:03:18,366 --> 00:03:19,966 is the largest one ever made, 47 00:03:20,046 --> 00:03:22,766 and new processes were required to manufacture it. 48 00:03:24,805 --> 00:03:29,285 The Orion heat shield has got to be able to withstand landing loads 49 00:03:29,365 --> 00:03:32,684 on the order of 300 to 400 thousand pounds. 50 00:03:32,764 --> 00:03:35,564 Because we're returning potentially from the Moon or beyond 51 00:03:35,643 --> 00:03:39,883 and the flight duration from the time in which you commit to a return 52 00:03:39,963 --> 00:03:41,403 to the time you actually land, 53 00:03:41,482 --> 00:03:44,682 the weather conditions on Earth can be substantially different 54 00:03:44,762 --> 00:03:46,002 or difficult to predict. 55 00:03:46,082 --> 00:03:49,081 And so the Orion spacecraft has to be able to land in the ocean 56 00:03:49,161 --> 00:03:51,601 in a wide range of sea conditions, 57 00:03:51,681 --> 00:03:55,280 wave height, wave slope angle and horizontal winds. 58 00:03:55,360 --> 00:03:59,959 That is what's driven us to a skin stringer architecture that utilizes 59 00:04:00,039 --> 00:04:04,998 a thick laminate composite skin bolted to a titanium sub-structure. 60 00:04:05,238 --> 00:04:08,718 We bond on an ablator, called the Avcoat. 61 00:04:08,798 --> 00:04:12,117 The ablator is the thermal protection part of the heat shield. 62 00:04:12,197 --> 00:04:14,877 The very outside of the ablator actually gets hot enough 63 00:04:14,957 --> 00:04:17,916 that it decomposes, and that's the ablation part of it, 64 00:04:17,996 --> 00:04:20,076 as opposed to an insulator like a shuttle tile. 65 00:04:22,995 --> 00:04:25,155 Then come the ancillary structures and equipment 66 00:04:25,235 --> 00:04:27,715 that will ride with the capsule. 67 00:04:27,795 --> 00:04:29,594 The escape tower, designed and tested, 68 00:04:29,674 --> 00:04:31,754 will pull the capsule away from the main rocket 69 00:04:31,834 --> 00:04:33,633 in the case of an emergency. 70 00:04:42,152 --> 00:04:45,911 Adaptor separation from the rocket's upper stage. 71 00:04:45,991 --> 00:04:48,191 Parachute deployment. 72 00:04:48,271 --> 00:04:50,511 The connecting adaptor to the EMS. 73 00:04:58,029 --> 00:05:01,469 The EMS is the service module attached to the Orion in flight, 74 00:05:01,549 --> 00:05:04,788 supplying oxygen, water, power and heating. 75 00:05:12,867 --> 00:05:16,786 Built by ESA, it is based on their very successful ATV program 76 00:05:16,866 --> 00:05:19,706 which delivered supplies to the ISS. 77 00:05:20,505 --> 00:05:24,625 It'll also provide the main engine thrust for deep space maneuvering. 78 00:05:41,102 --> 00:05:44,981 We have, in particular, a very, very tight schedule in front of us 79 00:05:45,061 --> 00:05:49,180 so everybody's working under high pressure to meet the dates 80 00:05:49,260 --> 00:05:52,500 and this requires a very, very close collaboration. 81 00:05:56,699 --> 00:06:01,738 I see a very motivated team, and so far, as an agency, 82 00:06:01,818 --> 00:06:04,778 we are quite happy with the performance of the European industry. 83 00:06:41,451 --> 00:06:45,171 The US Navy is tasked with retrieving the capsule from the ocean. 84 00:06:45,251 --> 00:06:48,610 At first they train in the pool, then calm waters, 85 00:06:48,690 --> 00:06:52,370 then the Pacific, and finally the real thing. 86 00:07:15,886 --> 00:07:18,845 Experts continue to evolve the process and training 87 00:07:18,925 --> 00:07:23,644 in readiness for the day when a manned flight returns from deep space. 88 00:07:38,362 --> 00:07:42,201 This is the RS-25, the Ferrari of liquid rocket engines 89 00:07:42,281 --> 00:07:45,000 and the main engine from the Space Shuttle program. 90 00:07:45,440 --> 00:07:48,000 Economically re-purposed for the Space Launch System, 91 00:07:48,080 --> 00:07:51,959 four of these engines will power the main stage of the rocket. 92 00:07:56,958 --> 00:07:59,278 The main solid rocket boosters of the shuttle program 93 00:07:59,358 --> 00:08:02,078 also have a renewed life in the SLS. 94 00:08:02,318 --> 00:08:03,957 With another two segments added, 95 00:08:04,037 --> 00:08:06,517 the boosters will thrust for over two minutes. 96 00:08:09,356 --> 00:08:11,956 This project has been a real fun effort in trying to take a heritage booster 97 00:08:14,715 --> 00:08:17,755 that had many, many years of reliability and great performance and evolve it into something bigger and better. 98 00:08:20,954 --> 00:08:22,834 When we first undertook this design 99 00:08:22,914 --> 00:08:24,714 and qualification for the new booster, 100 00:08:24,794 --> 00:08:28,273 part of the mission was to make the booster 101 00:08:28,353 --> 00:08:30,953 more affordable and more modern 102 00:08:31,033 --> 00:08:34,072 and, of course, it had to be completely redesigned for a new mission. 103 00:08:34,152 --> 00:08:35,512 It's a larger booster 104 00:08:35,592 --> 00:08:38,391 and the mission profile is sufficiently different 105 00:08:38,471 --> 00:08:41,751 to where pretty much everything on the inside of the booster is different. 106 00:08:41,831 --> 00:08:45,470 There's well over a thousand individual processes. 107 00:08:45,550 --> 00:08:48,470 Working with our customer, we were able to identify 108 00:08:48,550 --> 00:08:50,669 several hundred areas of improvement. 109 00:08:50,749 --> 00:08:53,909 We've got totally new avionics on this vehicle 110 00:08:53,989 --> 00:08:55,348 versus what we had on Shuttle. 111 00:08:55,428 --> 00:08:56,868 It's state of the art. 112 00:09:01,187 --> 00:09:03,987 Bigger and more powerful than any previous launch system, 113 00:09:04,067 --> 00:09:07,306 the SLS has been under development for some time. 114 00:09:07,986 --> 00:09:10,986 Designing it is one thing, building it another. 115 00:09:16,465 --> 00:09:19,344 In new or refurbished factories and assembly shops, 116 00:09:19,424 --> 00:09:24,943 the body of the largest rocket ever to fly is being constructed one piece at a time. 117 00:09:31,942 --> 00:09:34,022 The massive hydrogen tank takes shape. 118 00:10:07,176 --> 00:10:09,536 The smaller oxygen tank soon follows. 119 00:10:20,614 --> 00:10:24,253 The interim stage for the manned flight is another hydrogen-oxygen motor 120 00:10:24,333 --> 00:10:28,012 supplied by cryo tanks fabricated with new technologies. 121 00:10:32,132 --> 00:10:35,771 So to design and manufacture this tank, we used new materials. 122 00:10:35,851 --> 00:10:39,250 We processed the tank by automatic fiber placement. 123 00:10:39,330 --> 00:10:42,090 The benefit of that is we can lay down the material quickly, 124 00:10:42,170 --> 00:10:46,569 which provides us a low cost operation and a very lightweight tank. 125 00:10:47,289 --> 00:10:50,648 Well, we've worked on this program for 29 months and when we started, 126 00:10:50,728 --> 00:10:55,768 we'd never built a tank of this size by the methods that we did. 127 00:10:55,848 --> 00:11:00,207 We did automated fiber placement and fluted core, 128 00:11:00,887 --> 00:11:03,766 just developing the robotic fiber placement equipment 129 00:11:03,846 --> 00:11:06,806 in a way to make the skirt in one piece was a large challenge. 130 00:11:11,685 --> 00:11:14,364 Each exacting piece is fabricated, 131 00:11:14,444 --> 00:11:16,724 test articles are run through the mill, 132 00:11:16,804 --> 00:11:21,203 vibration tests, vacuum tests, acoustic tests, stress tests. 133 00:11:21,283 --> 00:11:23,283 Nothing is left to chance. 134 00:11:40,120 --> 00:11:45,559 New technology and new materials for a new generation of space exploration. 135 00:11:47,639 --> 00:11:49,798 For this test, there were several things that we looked at. 136 00:11:49,878 --> 00:11:53,158 This was the first time we used those thermal knives 137 00:11:53,238 --> 00:11:55,517 to start the deployment sequence. 138 00:11:55,597 --> 00:11:58,677 And that allowed cuts and tethers, 139 00:11:58,757 --> 00:12:02,156 but then allowed the solar array to deploy. 140 00:12:02,236 --> 00:12:06,355 We wanted to test the locking mechanisms to ensure that it locked properly in space 141 00:12:06,435 --> 00:12:11,994 because anything that could possibly go wrong, we wanted to see tested down here, 142 00:12:12,074 --> 00:12:15,354 so we can ensure, you know, a successful flight. 143 00:13:01,866 --> 00:13:03,226 It's all about technology. 144 00:13:03,306 --> 00:13:06,985 If you don't develop technologies for the future, 145 00:13:07,065 --> 00:13:09,025 you won't go where you want to go. 146 00:13:09,105 --> 00:13:13,424 So composites will decrease the weight of the tanks. 147 00:13:13,504 --> 00:13:16,783 It'll increase the payload performance of the launch vehicle. 148 00:13:16,863 --> 00:13:21,223 It'll give us-- it basically enables things that we don't have today. 149 00:13:24,902 --> 00:13:28,141 Soon the mighty rocket will lift human beings up further 150 00:13:28,221 --> 00:13:30,221 than ever before. 151 00:13:45,098 --> 00:13:50,218 The flight to Mars will be a long one, too long for a crew to sit in a capsule. 152 00:13:50,297 --> 00:13:54,577 A habitat and supplies will also be lifted to orbit and assembled. 153 00:13:54,657 --> 00:13:57,896 Several companies have been selected by NASA to carry out studies 154 00:13:57,976 --> 00:14:00,456 for a suitable system to do the job. 155 00:14:00,536 --> 00:14:03,655 A bit of competition is always good for invention. 156 00:14:05,015 --> 00:14:08,974 Bigelow Aerospace with its Expandable Activity Module, or BEAM, 157 00:14:09,054 --> 00:14:11,414 currently being tested on the ISS, 158 00:14:11,494 --> 00:14:14,493 will develop and test a prototype of XBASE, 159 00:14:14,573 --> 00:14:18,053 a 330 cubic meter expandable habitat. 160 00:14:18,773 --> 00:14:22,212 Boeing of Houston is developing a modular habitat system 161 00:14:22,292 --> 00:14:26,531 that leverages more than 15 years experience in designing, developing, 162 00:14:26,611 --> 00:14:27,931 assembling on-orbit, 163 00:14:28,011 --> 00:14:31,610 and safely operating the International Space Station. 164 00:14:32,650 --> 00:14:36,170 Lockheed Martin will refurbish a multi-purpose logistics module 165 00:14:36,250 --> 00:14:41,049 into a full-scale habitat prototype that will include integrated avionics 166 00:14:41,129 --> 00:14:42,968 and ECLSS. 167 00:14:43,928 --> 00:14:47,928 Orbital ATK will mature the mission architecture and design 168 00:14:48,008 --> 00:14:50,727 of their initial cislunar habitat concept, 169 00:14:50,807 --> 00:14:54,366 based on the Cygnus spacecraft that now supplies the ISS. 170 00:14:56,286 --> 00:15:00,045 Sierra Nevada Corporation's Space Systems will study and refine 171 00:15:00,125 --> 00:15:03,365 a flexible architecture and concept of operations 172 00:15:03,445 --> 00:15:06,444 for a deep space habitat that draws on the lessons 173 00:15:06,524 --> 00:15:11,683 of three to four commercial launches to construct a modular long-duration habitat. 174 00:15:13,443 --> 00:15:15,683 NanoRacks in conjunction with its partners, 175 00:15:15,763 --> 00:15:18,642 Space Systems Loral and the United Launch Alliance, 176 00:15:18,722 --> 00:15:21,882 referred to collectively as the Ixion Team, 177 00:15:21,962 --> 00:15:24,641 will conduct a comprehensive feasibility study 178 00:15:24,721 --> 00:15:28,361 regarding the conversion of an existing launch vehicle's upper stage, 179 00:15:28,441 --> 00:15:29,840 or propellant segment, 180 00:15:29,920 --> 00:15:33,400 into a pressurized habitable volume in space. 181 00:15:35,239 --> 00:15:38,959 So if you're designing spacecraft to be in the Mars orbit, 182 00:15:39,039 --> 00:15:42,438 then the studies we're doing on Space Station can be applied 183 00:15:42,518 --> 00:15:46,877 and help us to design more durable spacecraft for that Martian atmosphere. 184 00:15:46,957 --> 00:15:50,997 MISSE stands for the Materials International Space Station Experiment. 185 00:15:51,077 --> 00:15:56,676 We do study the durability of polymers in terms of their mechanical properties 186 00:15:56,756 --> 00:15:58,355 with radiation exposure. 187 00:15:58,435 --> 00:16:02,475 And we hear a lot about the radiation exposure impact on humans 188 00:16:02,555 --> 00:16:04,994 for flights to, say, Mars, 189 00:16:05,074 --> 00:16:08,154 but polymers and other materials that are used on spacecraft 190 00:16:08,234 --> 00:16:12,433 can also degrade from radiation and that's one of the things I study. 191 00:16:12,913 --> 00:16:17,432 The MISSE experiments do take a bit of time because we do very careful 192 00:16:17,512 --> 00:16:22,071 dehydration measurements of the samples after they've been in space. 193 00:16:22,151 --> 00:16:25,711 What we've found is that the Teflon erosion rate 194 00:16:25,791 --> 00:16:28,270 is highly dependent on the amount of sunlight 195 00:16:28,350 --> 00:16:30,630 and possibly the heating too. 196 00:16:30,710 --> 00:16:33,949 You need to know which of these environments it's gonna be exposed to 197 00:16:34,029 --> 00:16:38,149 because it'll erode at a different rate, depending on the environment. 198 00:16:39,188 --> 00:16:40,708 Assembling spacecraft in orbit 199 00:16:40,788 --> 00:16:44,907 and fueling them for the long journey to Mars sounds simple enough. 200 00:16:44,987 --> 00:16:48,587 On orbit, refueling is anything but simple. 201 00:16:50,466 --> 00:16:55,066 NASA have been developing a system for unmanned refueling for quite some time, 202 00:16:55,146 --> 00:16:58,465 and have a test article onboard the ISS. 203 00:17:02,304 --> 00:17:04,264 We can take a pick-and-place robot, 204 00:17:04,344 --> 00:17:06,624 put the tool wherever we need it to be, 205 00:17:06,704 --> 00:17:10,263 and all it needs to do is drive that tool because the smarts are in the tool. 206 00:17:10,343 --> 00:17:13,942 So, that's what we learned from working on Hubble is 207 00:17:14,022 --> 00:17:16,862 you put a smart tool with the astronauts 208 00:17:16,942 --> 00:17:18,662 and accomplish, you know, both things. 209 00:17:18,742 --> 00:17:20,781 You've got smart tools and astronauts working together. 210 00:17:20,861 --> 00:17:24,661 Now we're putting smart tools with robots and trying to accomplish 211 00:17:24,741 --> 00:17:26,740 the same type of things we did on Hubble. 212 00:17:26,820 --> 00:17:29,620 Aimed at developing capabilities for servicing, 213 00:17:29,700 --> 00:17:32,259 even refueling spacecraft on orbit, 214 00:17:32,339 --> 00:17:35,739 RRM is like doing precise surgery at a distance, 215 00:17:35,819 --> 00:17:39,538 doctor and patient separated by the void and vacuum of space. 216 00:17:39,618 --> 00:17:42,737 It's tough, but the payoff is huge. 217 00:17:42,897 --> 00:17:46,217 Robotics can do things that humans can't do 218 00:17:46,297 --> 00:17:48,576 in terms of precision, in terms of control. 219 00:17:48,656 --> 00:17:51,136 Holding a particular spot for six hours 220 00:17:51,216 --> 00:17:52,536 while engineers on the ground 221 00:17:52,616 --> 00:17:53,696 debate what to do. 222 00:17:53,775 --> 00:17:55,215 We can't ask a human to do that. 223 00:17:56,335 --> 00:17:59,654 The robot is a very stiff, rigid interface. 224 00:17:59,734 --> 00:18:02,414 It's not forgiving, like an astronaut's hand, 225 00:18:02,494 --> 00:18:04,374 so we have to take that into account. 226 00:18:05,493 --> 00:18:07,893 When you push on something really hard with the robot, 227 00:18:07,973 --> 00:18:09,773 you build up really large contact forces. 228 00:18:09,853 --> 00:18:12,652 When the astronaut pushes on something, his wrist might give-- 229 00:18:12,732 --> 00:18:16,692 you know, he's got his own internal software compliance running. 230 00:18:17,651 --> 00:18:20,811 But in order to accommodate the robot so we don't break anything, 231 00:18:20,891 --> 00:18:24,970 we have to build features into the tool, features into the software, 232 00:18:25,050 --> 00:18:28,090 just getting the robot to go where you want it to go. 233 00:18:28,170 --> 00:18:31,689 You know, they don't position precisely, so you have to do things like 234 00:18:31,769 --> 00:18:33,129 build lead-in into the tool. 235 00:18:33,209 --> 00:18:36,128 An astronaut can probably just get it right on there because he's right there. 236 00:18:36,208 --> 00:18:38,448 So we do have to do things to make them, you know, 237 00:18:38,528 --> 00:18:41,007 very specific to robotic operation. 238 00:18:41,567 --> 00:18:43,127 We're almost there. 239 00:18:50,606 --> 00:18:52,605 Whoa! 240 00:18:55,005 --> 00:18:59,564 That task successful, next stop Mars. 241 00:19:09,043 --> 00:19:12,642 The first manned mission to Mars will probably only orbit the planet, 242 00:19:12,722 --> 00:19:15,321 checking out all the gear and processes, 243 00:19:15,401 --> 00:19:19,361 even launching communication satellites and finalizing landing sites 244 00:19:19,441 --> 00:19:21,120 in preparation for the next mission, 245 00:19:21,200 --> 00:19:24,280 which will then make the descent to the surface. 246 00:19:24,520 --> 00:19:27,639 And that has a whole new set of problems to overcome. 247 00:19:29,039 --> 00:19:31,519 Unlike the moon, Mars has stronger gravity, 248 00:19:31,599 --> 00:19:33,518 about knot .6 of Earth's, 249 00:19:33,598 --> 00:19:37,198 but it does have an atmosphere where parachutes can be used, 250 00:19:37,278 --> 00:19:40,837 although the atmosphere is very thin and not very deep. 251 00:19:41,477 --> 00:19:43,956 Well, it's a funny thing about Mars, 252 00:19:44,036 --> 00:19:47,916 but if you take the average of the planet, 253 00:19:47,996 --> 00:19:50,715 the average height of everything in the planet, 254 00:19:50,795 --> 00:19:56,714 it turns out that most of the north is two kilometers below that 255 00:19:56,794 --> 00:20:00,034 and most of the south is two kilometers above that. 256 00:20:00,114 --> 00:20:04,993 And it's just, we always land in the north 'cause there's a lot more atmosphere. 257 00:20:05,073 --> 00:20:09,512 If you land in the south, it's like four kilometers less of air 258 00:20:09,592 --> 00:20:11,272 to come to a stop. 259 00:20:11,352 --> 00:20:16,591 In fact, at the altitude of the mountains in the south, 260 00:20:16,671 --> 00:20:19,910 the Mars science laboratory was still supersonic 261 00:20:19,990 --> 00:20:24,030 as it was descending into the crater it was reaching in the north. 262 00:20:26,669 --> 00:20:29,709 Assuming the need to pre-position habitats, supplies 263 00:20:29,789 --> 00:20:32,268 and equipment on the surface prior to humans landing, 264 00:20:32,348 --> 00:20:35,788 NASA and its partners are looking at several solutions. 265 00:20:37,987 --> 00:20:43,386 One is the HIAD or Hypersonic Inflatable Aerodynamic Decelerator. 266 00:20:43,466 --> 00:20:46,706 This is basically a very large inflatable heat shield, 267 00:20:46,786 --> 00:20:48,665 much larger in area than the payload, 268 00:20:48,745 --> 00:20:51,105 able to slow the craft considerably faster than a standard spacecraft heat shield. 269 00:20:54,424 --> 00:20:57,904 Plans are to test the system on a payload from the ISS, 270 00:20:57,984 --> 00:21:00,783 utilizing a Cygnus resupply spacecraft. 271 00:21:50,255 --> 00:21:54,334 Once lower in the atmosphere, parachutes will further slow the payload 272 00:21:54,414 --> 00:21:58,133 to an altitude low enough for rocket engines to take over. 273 00:22:09,251 --> 00:22:11,891 Morpheus and the Xombie flight systems have matured 274 00:22:11,971 --> 00:22:15,250 over the last few years and are capable of delivering cargo 275 00:22:15,330 --> 00:22:17,290 to a planet's surface autonomously, 276 00:22:17,370 --> 00:22:22,129 avoiding rough terrain or other obstacles without human intervention... 277 00:23:11,761 --> 00:23:15,480 ...adding yet another building block to our human effort 278 00:23:15,560 --> 00:23:17,640 to explore the solar system. 27211

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