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These are the user uploaded subtitles that are being translated: 1 00:00:03,840 --> 00:00:07,440 Our seafaring nature has translated well to the space age, 2 00:00:07,520 --> 00:00:11,800 sailing out into the unknown in search of riches of one kind or another. 3 00:00:12,840 --> 00:00:16,520 While Europe and Asia continue their interest in the resource-rich Moon, 4 00:00:16,600 --> 00:00:19,920 the United States and NASA have set their sights on nothing less 5 00:00:20,000 --> 00:00:22,200 than manned missions to Mars. 6 00:00:24,000 --> 00:00:26,000 Can they manage to go shore to shore 7 00:00:26,080 --> 00:00:29,720 on the most dangerous of unknown seas, deep space? 8 00:01:08,240 --> 00:01:12,480 With low Earth orbit harnessed, it is time to look further afield. 9 00:01:12,560 --> 00:01:15,200 To build a spacecraft and rocket system to reach Mars 10 00:01:15,280 --> 00:01:16,800 is a mammoth undertaking, 11 00:01:16,880 --> 00:01:19,480 but if successful, it will return the United States to the top of the space achievement ladder. 12 00:01:23,280 --> 00:01:24,640 The first requirement: 13 00:01:24,720 --> 00:01:28,680 a space capsule able to carry six astronauts for a long period of time 14 00:01:28,760 --> 00:01:31,000 and return them safely to Earth. 15 00:01:31,280 --> 00:01:35,640 Orion is its name and it has flown once already in a shakedown. 16 00:01:35,960 --> 00:01:39,680 The next flight will be an unmanned test mission past the moon, 17 00:01:39,760 --> 00:01:42,560 followed by a third manned mission. 18 00:01:45,040 --> 00:01:47,960 The components for the vehicle are developed around the country, 19 00:01:48,040 --> 00:01:51,320 tested and checked, then passed on for assembly. 20 00:01:51,400 --> 00:01:55,000 The minutest bolt and circuit is designed, tested, redesigned 21 00:01:55,080 --> 00:01:56,280 and tested again. 22 00:01:57,000 --> 00:01:58,720 Slowly the systems come together, 23 00:01:58,800 --> 00:02:01,480 with the aid of some breakthrough technology, 24 00:02:01,560 --> 00:02:05,800 particularly in manufacturing methods, new materials and processes. 25 00:02:06,400 --> 00:02:09,120 The first thing to notice is that NASA have gone back 26 00:02:09,200 --> 00:02:13,720 to the classic conic shape like Apollo, the safest design yet devised. 27 00:02:14,200 --> 00:02:18,760 Avionics, control systems, computer software and a glass cockpit, 28 00:02:18,840 --> 00:02:20,840 all state of the art. 29 00:02:25,000 --> 00:02:27,920 ...and the concept was to go with a glass cockpit 30 00:02:28,000 --> 00:02:32,000 and what that means is that the instruments are all images 31 00:02:32,080 --> 00:02:33,040 on a computer screen. 32 00:02:33,120 --> 00:02:37,560 They are all on glass, so rather than flipping a physical switch, 33 00:02:37,640 --> 00:02:41,480 the crew brings up a computer screen and flips a virtual switch, 34 00:02:41,560 --> 00:02:44,400 a little icon of a switch or icon of a valve, 35 00:02:44,480 --> 00:02:49,480 and with the exception of seven panels right around the computer screens, 36 00:02:49,560 --> 00:02:51,560 which have about 60 switches, 37 00:02:51,640 --> 00:02:55,920 that is all of the cockpit of Orion happens on the glass. 38 00:02:56,000 --> 00:02:57,840 One big benefit is the weight savings 39 00:02:57,920 --> 00:03:00,200 because you don't have to have a physical switch. 40 00:03:00,280 --> 00:03:01,680 And having a physical switch, 41 00:03:01,760 --> 00:03:03,960 not only is there the weight of the switch, 42 00:03:04,040 --> 00:03:07,040 but you also have the weight of the wire to the switch, 43 00:03:07,120 --> 00:03:10,680 and you have to have the weight of circuitry that takes that wire 44 00:03:10,760 --> 00:03:13,520 and feeds it into the vehicle computers. 45 00:03:15,240 --> 00:03:18,160 Because of Orion's size, its all-important heat shield 46 00:03:18,240 --> 00:03:19,840 is the largest one ever made, 47 00:03:19,920 --> 00:03:22,640 and new processes were required to manufacture it. 48 00:03:24,680 --> 00:03:29,160 The Orion heat shield has got to be able to withstand landing loads 49 00:03:29,240 --> 00:03:32,560 on the order of 300 to 400 thousand pounds. 50 00:03:32,640 --> 00:03:35,440 Because we're returning potentially from the Moon or beyond 51 00:03:35,520 --> 00:03:39,760 and the flight duration from the time in which you commit to a return 52 00:03:39,840 --> 00:03:41,280 to the time you actually land, 53 00:03:41,360 --> 00:03:44,560 the weather conditions on Earth can be substantially different 54 00:03:44,640 --> 00:03:45,880 or difficult to predict. 55 00:03:45,960 --> 00:03:48,960 And so the Orion spacecraft has to be able to land in the ocean 56 00:03:49,040 --> 00:03:51,480 in a wide range of sea conditions, 57 00:03:51,560 --> 00:03:55,160 wave height, wave slope angle and horizontal winds. 58 00:03:55,240 --> 00:03:59,840 That is what's driven us to a skin stringer architecture that utilizes 59 00:03:59,920 --> 00:04:04,880 a thick laminate composite skin bolted to a titanium sub-structure. 60 00:04:05,120 --> 00:04:08,600 We bond on an ablator, called the Avcoat. 61 00:04:08,680 --> 00:04:12,000 The ablator is the thermal protection part of the heat shield. 62 00:04:12,080 --> 00:04:14,760 The very outside of the ablator actually gets hot enough 63 00:04:14,840 --> 00:04:17,800 that it decomposes, and that's the ablation part of it, 64 00:04:17,880 --> 00:04:19,960 as opposed to an insulator like a shuttle tile. 65 00:04:22,880 --> 00:04:25,040 Then come the ancillary structures and equipment 66 00:04:25,120 --> 00:04:27,600 that will ride with the capsule. 67 00:04:27,680 --> 00:04:29,480 The escape tower, designed and tested, 68 00:04:29,560 --> 00:04:31,640 will pull the capsule away from the main rocket 69 00:04:31,720 --> 00:04:33,520 in the case of an emergency. 70 00:04:42,040 --> 00:04:45,800 Adaptor separation from the rocket's upper stage. 71 00:04:45,880 --> 00:04:48,080 Parachute deployment. 72 00:04:48,160 --> 00:04:50,400 The connecting adaptor to the EMS. 73 00:04:57,920 --> 00:05:01,360 The EMS is the service module attached to the Orion in flight, 74 00:05:01,440 --> 00:05:04,680 supplying oxygen, water, power and heating. 75 00:05:12,760 --> 00:05:16,680 Built by ESA, it is based on their very successful ATV program 76 00:05:16,760 --> 00:05:19,600 which delivered supplies to the ISS. 77 00:05:20,400 --> 00:05:24,520 It'll also provide the main engine thrust for deep space maneuvering. 78 00:05:41,000 --> 00:05:44,880 We have, in particular, a very, very tight schedule in front of us 79 00:05:44,960 --> 00:05:49,080 so everybody's working under high pressure to meet the dates 80 00:05:49,160 --> 00:05:52,400 and this requires a very, very close collaboration. 81 00:05:56,600 --> 00:06:01,640 I see a very motivated team, and so far, as an agency, 82 00:06:01,720 --> 00:06:04,680 we are quite happy with the performance of the European industry. 83 00:06:41,360 --> 00:06:45,080 The US Navy is tasked with retrieving the capsule from the ocean. 84 00:06:45,160 --> 00:06:48,520 At first they train in the pool, then calm waters, 85 00:06:48,600 --> 00:06:52,280 then the Pacific, and finally the real thing. 86 00:07:15,800 --> 00:07:18,760 Experts continue to evolve the process and training 87 00:07:18,840 --> 00:07:23,560 in readiness for the day when a manned flight returns from deep space. 88 00:07:38,280 --> 00:07:42,120 This is the RS-25, the Ferrari of liquid rocket engines 89 00:07:42,200 --> 00:07:44,920 and the main engine from the Space Shuttle program. 90 00:07:45,360 --> 00:07:47,920 Economically re-purposed for the Space Launch System, 91 00:07:48,000 --> 00:07:51,880 four of these engines will power the main stage of the rocket. 92 00:07:56,880 --> 00:07:59,200 The main solid rocket boosters of the shuttle program 93 00:07:59,280 --> 00:08:02,000 also have a renewed life in the SLS. 94 00:08:02,240 --> 00:08:03,880 With another two segments added, 95 00:08:03,960 --> 00:08:06,440 the boosters will thrust for over two minutes. 96 00:08:09,280 --> 00:08:11,880 This project has been a real fun effort in trying to take a heritage booster 97 00:08:14,640 --> 00:08:17,680 that had many, many years of reliability and great performance and evolve it into something bigger and better. 98 00:08:20,880 --> 00:08:22,760 When we first undertook this design 99 00:08:22,840 --> 00:08:24,640 and qualification for the new booster, 100 00:08:24,720 --> 00:08:28,200 part of the mission was to make the booster 101 00:08:28,280 --> 00:08:30,880 more affordable and more modern 102 00:08:30,960 --> 00:08:34,000 and, of course, it had to be completely redesigned for a new mission. 103 00:08:34,080 --> 00:08:35,440 It's a larger booster 104 00:08:35,520 --> 00:08:38,320 and the mission profile is sufficiently different 105 00:08:38,400 --> 00:08:41,680 to where pretty much everything on the inside of the booster is different. 106 00:08:41,760 --> 00:08:45,400 There's well over a thousand individual processes. 107 00:08:45,480 --> 00:08:48,400 Working with our customer, we were able to identify 108 00:08:48,480 --> 00:08:50,600 several hundred areas of improvement. 109 00:08:50,680 --> 00:08:53,840 We've got totally new avionics on this vehicle 110 00:08:53,920 --> 00:08:55,280 versus what we had on Shuttle. 111 00:08:55,360 --> 00:08:56,800 It's state of the art. 112 00:09:01,120 --> 00:09:03,920 Bigger and more powerful than any previous launch system, 113 00:09:04,000 --> 00:09:07,240 the SLS has been under development for some time. 114 00:09:07,920 --> 00:09:10,920 Designing it is one thing, building it another. 115 00:09:16,400 --> 00:09:19,280 In new or refurbished factories and assembly shops, 116 00:09:19,360 --> 00:09:24,880 the body of the largest rocket ever to fly is being constructed one piece at a time. 117 00:09:31,880 --> 00:09:33,960 The massive hydrogen tank takes shape. 118 00:10:07,120 --> 00:10:09,480 The smaller oxygen tank soon follows. 119 00:10:20,560 --> 00:10:24,200 The interim stage for the manned flight is another hydrogen-oxygen motor 120 00:10:24,280 --> 00:10:27,960 supplied by cryo tanks fabricated with new technologies. 121 00:10:32,080 --> 00:10:35,720 So to design and manufacture this tank, we used new materials. 122 00:10:35,800 --> 00:10:39,200 We processed the tank by automatic fiber placement. 123 00:10:39,280 --> 00:10:42,040 The benefit of that is we can lay down the material quickly, 124 00:10:42,120 --> 00:10:46,520 which provides us a low cost operation and a very lightweight tank. 125 00:10:47,240 --> 00:10:50,600 Well, we've worked on this program for 29 months and when we started, 126 00:10:50,680 --> 00:10:55,720 we'd never built a tank of this size by the methods that we did. 127 00:10:55,800 --> 00:11:00,160 We did automated fiber placement and fluted core, 128 00:11:00,840 --> 00:11:03,720 just developing the robotic fiber placement equipment 129 00:11:03,800 --> 00:11:06,760 in a way to make the skirt in one piece was a large challenge. 130 00:11:11,640 --> 00:11:14,320 Each exacting piece is fabricated, 131 00:11:14,400 --> 00:11:16,680 test articles are run through the mill, 132 00:11:16,760 --> 00:11:21,160 vibration tests, vacuum tests, acoustic tests, stress tests. 133 00:11:21,240 --> 00:11:23,240 Nothing is left to chance. 134 00:11:40,080 --> 00:11:45,520 New technology and new materials for a new generation of space exploration. 135 00:11:47,600 --> 00:11:49,760 For this test, there were several things that we looked at. 136 00:11:49,840 --> 00:11:53,120 This was the first time we used those thermal knives 137 00:11:53,200 --> 00:11:55,480 to start the deployment sequence. 138 00:11:55,560 --> 00:11:58,640 And that allowed cuts and tethers, 139 00:11:58,720 --> 00:12:02,120 but then allowed the solar array to deploy. 140 00:12:02,200 --> 00:12:06,320 We wanted to test the locking mechanisms to ensure that it locked properly in space 141 00:12:06,400 --> 00:12:11,960 because anything that could possibly go wrong, we wanted to see tested down here, 142 00:12:12,040 --> 00:12:15,320 so we can ensure, you know, a successful flight. 143 00:13:01,840 --> 00:13:03,200 It's all about technology. 144 00:13:03,280 --> 00:13:06,960 If you don't develop technologies for the future, 145 00:13:07,040 --> 00:13:09,000 you won't go where you want to go. 146 00:13:09,080 --> 00:13:13,400 So composites will decrease the weight of the tanks. 147 00:13:13,480 --> 00:13:16,760 It'll increase the payload performance of the launch vehicle. 148 00:13:16,840 --> 00:13:21,200 It'll give us-- it basically enables things that we don't have today. 149 00:13:24,880 --> 00:13:28,120 Soon the mighty rocket will lift human beings up further 150 00:13:28,200 --> 00:13:30,200 than ever before. 151 00:13:45,080 --> 00:13:50,200 The flight to Mars will be a long one, too long for a crew to sit in a capsule. 152 00:13:50,280 --> 00:13:54,560 A habitat and supplies will also be lifted to orbit and assembled. 153 00:13:54,640 --> 00:13:57,880 Several companies have been selected by NASA to carry out studies 154 00:13:57,960 --> 00:14:00,440 for a suitable system to do the job. 155 00:14:00,520 --> 00:14:03,640 A bit of competition is always good for invention. 156 00:14:05,000 --> 00:14:08,960 Bigelow Aerospace with its Expandable Activity Module, or BEAM, 157 00:14:09,040 --> 00:14:11,400 currently being tested on the ISS, 158 00:14:11,480 --> 00:14:14,480 will develop and test a prototype of XBASE, 159 00:14:14,560 --> 00:14:18,040 a 330 cubic meter expandable habitat. 160 00:14:18,760 --> 00:14:22,200 Boeing of Houston is developing a modular habitat system 161 00:14:22,280 --> 00:14:26,520 that leverages more than 15 years experience in designing, developing, 162 00:14:26,600 --> 00:14:27,920 assembling on-orbit, 163 00:14:28,000 --> 00:14:31,600 and safely operating the International Space Station. 164 00:14:32,640 --> 00:14:36,160 Lockheed Martin will refurbish a multi-purpose logistics module 165 00:14:36,240 --> 00:14:41,040 into a full-scale habitat prototype that will include integrated avionics 166 00:14:41,120 --> 00:14:42,960 and ECLSS. 167 00:14:43,920 --> 00:14:47,920 Orbital ATK will mature the mission architecture and design 168 00:14:48,000 --> 00:14:50,720 of their initial cislunar habitat concept, 169 00:14:50,800 --> 00:14:54,360 based on the Cygnus spacecraft that now supplies the ISS. 170 00:14:56,280 --> 00:15:00,040 Sierra Nevada Corporation's Space Systems will study and refine 171 00:15:00,120 --> 00:15:03,360 a flexible architecture and concept of operations 172 00:15:03,440 --> 00:15:06,440 for a deep space habitat that draws on the lessons 173 00:15:06,520 --> 00:15:11,680 of three to four commercial launches to construct a modular long-duration habitat. 174 00:15:13,440 --> 00:15:15,680 NanoRacks in conjunction with its partners, 175 00:15:15,760 --> 00:15:18,640 Space Systems Loral and the United Launch Alliance, 176 00:15:18,720 --> 00:15:21,880 referred to collectively as the Ixion Team, 177 00:15:21,960 --> 00:15:24,640 will conduct a comprehensive feasibility study 178 00:15:24,720 --> 00:15:28,360 regarding the conversion of an existing launch vehicle's upper stage, 179 00:15:28,440 --> 00:15:29,840 or propellant segment, 180 00:15:29,920 --> 00:15:33,400 into a pressurized habitable volume in space. 181 00:15:35,240 --> 00:15:38,960 So if you're designing spacecraft to be in the Mars orbit, 182 00:15:39,040 --> 00:15:42,440 then the studies we're doing on Space Station can be applied 183 00:15:42,520 --> 00:15:46,880 and help us to design more durable spacecraft for that Martian atmosphere. 184 00:15:46,960 --> 00:15:51,000 MISSE stands for the Materials International Space Station Experiment. 185 00:15:51,080 --> 00:15:56,680 We do study the durability of polymers in terms of their mechanical properties 186 00:15:56,760 --> 00:15:58,360 with radiation exposure. 187 00:15:58,440 --> 00:16:02,480 And we hear a lot about the radiation exposure impact on humans 188 00:16:02,560 --> 00:16:05,000 for flights to, say, Mars, 189 00:16:05,080 --> 00:16:08,160 but polymers and other materials that are used on spacecraft 190 00:16:08,240 --> 00:16:12,440 can also degrade from radiation and that's one of the things I study. 191 00:16:12,920 --> 00:16:17,440 The MISSE experiments do take a bit of time because we do very careful 192 00:16:17,520 --> 00:16:22,080 dehydration measurements of the samples after they've been in space. 193 00:16:22,160 --> 00:16:25,720 What we've found is that the Teflon erosion rate 194 00:16:25,800 --> 00:16:28,280 is highly dependent on the amount of sunlight 195 00:16:28,360 --> 00:16:30,640 and possibly the heating too. 196 00:16:30,720 --> 00:16:33,960 You need to know which of these environments it's gonna be exposed to 197 00:16:34,040 --> 00:16:38,160 because it'll erode at a different rate, depending on the environment. 198 00:16:39,200 --> 00:16:40,720 Assembling spacecraft in orbit 199 00:16:40,800 --> 00:16:44,920 and fueling them for the long journey to Mars sounds simple enough. 200 00:16:45,000 --> 00:16:48,600 On orbit, refueling is anything but simple. 201 00:16:50,480 --> 00:16:55,080 NASA have been developing a system for unmanned refueling for quite some time, 202 00:16:55,160 --> 00:16:58,480 and have a test article onboard the ISS. 203 00:17:02,320 --> 00:17:04,280 We can take a pick-and-place robot, 204 00:17:04,360 --> 00:17:06,640 put the tool wherever we need it to be, 205 00:17:06,720 --> 00:17:10,280 and all it needs to do is drive that tool because the smarts are in the tool. 206 00:17:10,360 --> 00:17:13,960 So, that's what we learned from working on Hubble is 207 00:17:14,040 --> 00:17:16,880 you put a smart tool with the astronauts 208 00:17:16,960 --> 00:17:18,680 and accomplish, you know, both things. 209 00:17:18,760 --> 00:17:20,800 You've got smart tools and astronauts working together. 210 00:17:20,880 --> 00:17:24,680 Now we're putting smart tools with robots and trying to accomplish 211 00:17:24,760 --> 00:17:26,760 the same type of things we did on Hubble. 212 00:17:26,840 --> 00:17:29,640 Aimed at developing capabilities for servicing, 213 00:17:29,720 --> 00:17:32,280 even refueling spacecraft on orbit, 214 00:17:32,360 --> 00:17:35,760 RRM is like doing precise surgery at a distance, 215 00:17:35,840 --> 00:17:39,560 doctor and patient separated by the void and vacuum of space. 216 00:17:39,640 --> 00:17:42,760 It's tough, but the payoff is huge. 217 00:17:42,920 --> 00:17:46,240 Robotics can do things that humans can't do 218 00:17:46,320 --> 00:17:48,600 in terms of precision, in terms of control. 219 00:17:48,680 --> 00:17:51,160 Holding a particular spot for six hours 220 00:17:51,240 --> 00:17:52,560 while engineers on the ground 221 00:17:52,640 --> 00:17:53,720 debate what to do. 222 00:17:53,800 --> 00:17:55,240 We can't ask a human to do that. 223 00:17:56,360 --> 00:17:59,680 The robot is a very stiff, rigid interface. 224 00:17:59,760 --> 00:18:02,440 It's not forgiving, like an astronaut's hand, 225 00:18:02,520 --> 00:18:04,400 so we have to take that into account. 226 00:18:05,520 --> 00:18:07,920 When you push on something really hard with the robot, 227 00:18:08,000 --> 00:18:09,800 you build up really large contact forces. 228 00:18:09,880 --> 00:18:12,680 When the astronaut pushes on something, his wrist might give-- 229 00:18:12,760 --> 00:18:16,720 you know, he's got his own internal software compliance running. 230 00:18:17,680 --> 00:18:20,840 But in order to accommodate the robot so we don't break anything, 231 00:18:20,920 --> 00:18:25,000 we have to build features into the tool, features into the software, 232 00:18:25,080 --> 00:18:28,120 just getting the robot to go where you want it to go. 233 00:18:28,200 --> 00:18:31,720 You know, they don't position precisely, so you have to do things like 234 00:18:31,800 --> 00:18:33,160 build lead-in into the tool. 235 00:18:33,240 --> 00:18:36,160 An astronaut can probably just get it right on there because he's right there. 236 00:18:36,240 --> 00:18:38,480 So we do have to do things to make them, you know, 237 00:18:38,560 --> 00:18:41,040 very specific to robotic operation. 238 00:18:41,600 --> 00:18:43,160 We're almost there. 239 00:18:50,640 --> 00:18:52,640 Whoa! 240 00:18:55,040 --> 00:18:59,600 That task successful, next stop Mars. 241 00:19:09,080 --> 00:19:12,680 The first manned mission to Mars will probably only orbit the planet, 242 00:19:12,760 --> 00:19:15,360 checking out all the gear and processes, 243 00:19:15,440 --> 00:19:19,400 even launching communication satellites and finalizing landing sites 244 00:19:19,480 --> 00:19:21,160 in preparation for the next mission, 245 00:19:21,240 --> 00:19:24,320 which will then make the descent to the surface. 246 00:19:24,560 --> 00:19:27,680 And that has a whole new set of problems to overcome. 247 00:19:29,080 --> 00:19:31,560 Unlike the moon, Mars has stronger gravity, 248 00:19:31,640 --> 00:19:33,560 about knot .6 of Earth's, 249 00:19:33,640 --> 00:19:37,240 but it does have an atmosphere where parachutes can be used, 250 00:19:37,320 --> 00:19:40,880 although the atmosphere is very thin and not very deep. 251 00:19:41,520 --> 00:19:44,000 Well, it's a funny thing about Mars, 252 00:19:44,080 --> 00:19:47,960 but if you take the average of the planet, 253 00:19:48,040 --> 00:19:50,760 the average height of everything in the planet, 254 00:19:50,840 --> 00:19:56,760 it turns out that most of the north is two kilometers below that 255 00:19:56,840 --> 00:20:00,080 and most of the south is two kilometers above that. 256 00:20:00,160 --> 00:20:05,040 And it's just, we always land in the north 'cause there's a lot more atmosphere. 257 00:20:05,120 --> 00:20:09,560 If you land in the south, it's like four kilometers less of air 258 00:20:09,640 --> 00:20:11,320 to come to a stop. 259 00:20:11,400 --> 00:20:16,640 In fact, at the altitude of the mountains in the south, 260 00:20:16,720 --> 00:20:19,960 the Mars science laboratory was still supersonic 261 00:20:20,040 --> 00:20:24,080 as it was descending into the crater it was reaching in the north. 262 00:20:26,720 --> 00:20:29,760 Assuming the need to pre-position habitats, supplies 263 00:20:29,840 --> 00:20:32,320 and equipment on the surface prior to humans landing, 264 00:20:32,400 --> 00:20:35,840 NASA and its partners are looking at several solutions. 265 00:20:38,040 --> 00:20:43,440 One is the HIAD or Hypersonic Inflatable Aerodynamic Decelerator. 266 00:20:43,520 --> 00:20:46,760 This is basically a very large inflatable heat shield, 267 00:20:46,840 --> 00:20:48,720 much larger in area than the payload, 268 00:20:48,800 --> 00:20:51,160 able to slow the craft considerably faster than a standard spacecraft heat shield. 269 00:20:54,480 --> 00:20:57,960 Plans are to test the system on a payload from the ISS, 270 00:20:58,040 --> 00:21:00,840 utilizing a Cygnus resupply spacecraft. 271 00:21:50,320 --> 00:21:54,400 Once lower in the atmosphere, parachutes will further slow the payload 272 00:21:54,480 --> 00:21:58,200 to an altitude low enough for rocket engines to take over. 273 00:22:09,320 --> 00:22:11,960 Morpheus and the Xombie flight systems have matured 274 00:22:12,040 --> 00:22:15,320 over the last few years and are capable of delivering cargo 275 00:22:15,400 --> 00:22:17,360 to a planet's surface autonomously, 276 00:22:17,440 --> 00:22:22,200 avoiding rough terrain or other obstacles without human intervention... 277 00:23:11,840 --> 00:23:15,560 ...adding yet another building block to our human effort 278 00:23:15,640 --> 00:23:17,720 to explore the solar system. 27211

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