1 00:00:11,749 --> 00:00:09,430 the more recent soyuz crews have been 2 00:00:13,910 --> 00:00:11,759 taking six hour trips um to the 3 00:00:15,509 --> 00:00:13,920 international space station this one's 4 00:00:19,269 --> 00:00:15,519 taking two days and that's to test out 5 00:00:21,189 --> 00:00:19,279 the variety of upgrades that have been 6 00:00:23,349 --> 00:00:21,199 added to the newly modified soyuz 7 00:00:26,070 --> 00:00:23,359 vehicle this includes thrusters debris 8 00:00:28,230 --> 00:00:26,080 shielding power and digital video 9 00:00:30,390 --> 00:00:28,240 as well as many other things 10 00:00:33,350 --> 00:00:30,400 but what makes this soyuz so different 11 00:00:34,630 --> 00:00:33,360 from uh other previous models 12 00:00:38,950 --> 00:00:34,640 a few 13 00:00:40,389 --> 00:00:38,960 sat down with mark bowman the chief 14 00:00:41,990 --> 00:00:40,399 engineer of the soyuz branch of the 15 00:00:45,110 --> 00:00:42,000 astronaut office here at the johnson 16 00:00:47,350 --> 00:00:45,120 space center to find out and he asked 17 00:00:49,510 --> 00:00:47,360 bowman to begin by explaining the goals 18 00:00:51,189 --> 00:00:49,520 of the russian designers had in mind 19 00:00:55,990 --> 00:00:51,199 when they set out to improve this 20 00:00:59,910 --> 00:00:58,310 they stated two major reasons for 21 00:01:01,590 --> 00:00:59,920 performing the modifications the first 22 00:01:03,910 --> 00:01:01,600 is to increase the reliability of the 23 00:01:06,870 --> 00:01:03,920 spacecraft and the second is to enhance 24 00:01:09,109 --> 00:01:06,880 performance and technical specifications 25 00:01:11,030 --> 00:01:09,119 there were a lot of changes the first is 26 00:01:13,109 --> 00:01:11,040 a structural change they added 27 00:01:15,429 --> 00:01:13,119 additional shielding for micro meteorite 28 00:01:17,190 --> 00:01:15,439 and orbital debris to the habitation 29 00:01:19,749 --> 00:01:17,200 module and the intent of this is to 30 00:01:22,630 --> 00:01:19,759 increase what we in space parlance call 31 00:01:24,550 --> 00:01:22,640 the probability of non-penetration in 32 00:01:26,310 --> 00:01:24,560 other words to reduce the chance that a 33 00:01:28,149 --> 00:01:26,320 micro meteorite or some piece of orbital 34 00:01:30,069 --> 00:01:28,159 debris would actually punch a hole 35 00:01:32,149 --> 00:01:30,079 through the spacecraft 36 00:01:34,149 --> 00:01:32,159 the second change is a modification to 37 00:01:37,429 --> 00:01:34,159 the electrical power system 38 00:01:39,030 --> 00:01:37,439 to increase the the reserves of power 39 00:01:42,149 --> 00:01:39,040 the first thing they did was to add a 40 00:01:43,749 --> 00:01:42,159 fifth battery assembly to the spacecraft 41 00:01:45,590 --> 00:01:43,759 each battery assembly consists of a 42 00:01:48,469 --> 00:01:45,600 prime battery and a backup battery so by 43 00:01:50,389 --> 00:01:48,479 adding a fifth unit that's a 20 increase 44 00:01:53,190 --> 00:01:50,399 in the energy storage capacity on the 45 00:01:54,789 --> 00:01:53,200 spacecraft and to provide the power that 46 00:01:57,030 --> 00:01:54,799 go into those batteries there are solar 47 00:01:59,270 --> 00:01:57,040 arrays on the spacecraft and they added 48 00:02:01,350 --> 00:01:59,280 some additional surface area of the 49 00:02:03,429 --> 00:02:01,360 photoelectric cells on the solar arrays 50 00:02:06,069 --> 00:02:03,439 which increased surface area by a little 51 00:02:08,309 --> 00:02:06,079 over a square meter of area and they 52 00:02:10,229 --> 00:02:08,319 used additional or modern photoelectric 53 00:02:12,550 --> 00:02:10,239 cells on those arrays to increase the 54 00:02:15,190 --> 00:02:12,560 efficiency by about two percent so that 55 00:02:16,550 --> 00:02:15,200 helps to increase the power reserves on 56 00:02:18,949 --> 00:02:16,560 the spacecraft 57 00:02:20,710 --> 00:02:18,959 in addition they change the telemetry 58 00:02:22,630 --> 00:02:20,720 system the radio system that sends 59 00:02:24,790 --> 00:02:22,640 telemetry down to the ground and 60 00:02:26,790 --> 00:02:24,800 receives commands from the ground in the 61 00:02:28,710 --> 00:02:26,800 spacecraft to go to a much more modern 62 00:02:29,830 --> 00:02:28,720 system what they're calling an 63 00:02:32,630 --> 00:02:29,840 integrated 64 00:02:35,270 --> 00:02:32,640 command and telemetry system this makes 65 00:02:36,869 --> 00:02:35,280 use of the new russian looch satellites 66 00:02:39,430 --> 00:02:36,879 which are analogous to our tracking and 67 00:02:41,750 --> 00:02:39,440 data relay satellites and will greatly 68 00:02:43,750 --> 00:02:41,760 increase the amount of coverage that the 69 00:02:45,670 --> 00:02:43,760 communications systems on the spacecraft 70 00:02:47,430 --> 00:02:45,680 so ground controllers would be able to 71 00:02:49,990 --> 00:02:47,440 send commands as you know now they can 72 00:02:52,470 --> 00:02:50,000 only command to the spacecraft for about 73 00:02:53,910 --> 00:02:52,480 a maximum of 20 minutes per orbit and 74 00:02:55,430 --> 00:02:53,920 that's when they happen to be in an 75 00:02:56,390 --> 00:02:55,440 orbit that goes over a russian ground 76 00:02:58,070 --> 00:02:56,400 station 77 00:03:00,229 --> 00:02:58,080 once this system is fully up and running 78 00:03:03,030 --> 00:03:00,239 and tested they'll be able to send 79 00:03:05,430 --> 00:03:03,040 commands for at least 45 percent to 80 00:03:06,710 --> 00:03:05,440 perhaps 80 or 90 percent of an orbital 81 00:03:08,790 --> 00:03:06,720 coverage 82 00:03:11,670 --> 00:03:08,800 as also as part of that yakitaya system 83 00:03:13,509 --> 00:03:11,680 they've transitioned to an s-band system 84 00:03:16,229 --> 00:03:13,519 they removed the old antennas that 85 00:03:17,910 --> 00:03:16,239 supported the the old radio system and 86 00:03:20,790 --> 00:03:17,920 replaced those with four 87 00:03:22,390 --> 00:03:20,800 omni-directional antennas that provide 88 00:03:24,630 --> 00:03:22,400 access to the spacecraft from all of the 89 00:03:27,270 --> 00:03:24,640 russian ground sites and additionally 90 00:03:29,670 --> 00:03:27,280 they added a phased array antenna that 91 00:03:31,750 --> 00:03:29,680 will point at the looch satellites which 92 00:03:33,910 --> 00:03:31,760 are in geosynchronous orbit so phase 93 00:03:35,750 --> 00:03:33,920 deray antenna allows them to point more 94 00:03:38,229 --> 00:03:35,760 precisely to 95 00:03:40,070 --> 00:03:38,239 get communication with those satellites 96 00:03:42,470 --> 00:03:40,080 they also improve the communication 97 00:03:44,470 --> 00:03:42,480 system the vhf communications radios in 98 00:03:46,390 --> 00:03:44,480 the descent module which the crew 99 00:03:48,949 --> 00:03:46,400 members used for voice communications 100 00:03:50,789 --> 00:03:48,959 with the ground um the yakata system 101 00:03:53,270 --> 00:03:50,799 includes a backup capability that will 102 00:03:56,309 --> 00:03:53,280 eventually enable them to have ground 103 00:03:58,070 --> 00:03:56,319 voice command voice communications 104 00:04:00,470 --> 00:03:58,080 in addition to vhf but that's not 105 00:04:02,949 --> 00:04:00,480 functional yet on this first spacecraft 106 00:04:05,190 --> 00:04:02,959 but the improvements to the vhf radios 107 00:04:07,190 --> 00:04:05,200 in the descent module provide provide a 108 00:04:09,990 --> 00:04:07,200 lot of additional safety to the crew 109 00:04:12,470 --> 00:04:10,000 members because they've added a global 110 00:04:14,789 --> 00:04:12,480 positioning satellite receiver on the 111 00:04:16,710 --> 00:04:14,799 hatch of the spacecraft so once the 112 00:04:18,949 --> 00:04:16,720 parachutes have opened during re-entry 113 00:04:21,189 --> 00:04:18,959 they start taking data from a gps which 114 00:04:23,590 --> 00:04:21,199 tells the spacecraft where it's located 115 00:04:25,590 --> 00:04:23,600 then the radio system also has a new 116 00:04:27,110 --> 00:04:25,600 transponder that sends then that 117 00:04:29,830 --> 00:04:27,120 location to 118 00:04:31,590 --> 00:04:29,840 the coast bar and sarsat rescue 119 00:04:33,350 --> 00:04:31,600 satellite systems it's a universal 120 00:04:34,710 --> 00:04:33,360 system that's used all over the world 121 00:04:36,550 --> 00:04:34,720 and this will allow the search and 122 00:04:38,710 --> 00:04:36,560 rescue crews to quickly locate a 123 00:04:41,030 --> 00:04:38,720 spacecraft in the event say of bad 124 00:04:43,510 --> 00:04:41,040 weather or a ballistic entry so it 125 00:04:45,030 --> 00:04:43,520 greatly improves the the reliability the 126 00:04:47,189 --> 00:04:45,040 other thing they did was change the 127 00:04:49,590 --> 00:04:47,199 coors rendezvous radar system which has 128 00:04:52,390 --> 00:04:49,600 been used for many years on the soyuz 129 00:04:55,430 --> 00:04:52,400 the new coors includes much upgraded 130 00:04:57,510 --> 00:04:55,440 avionics modernized electronic systems 131 00:04:59,909 --> 00:04:57,520 new antennas they have actually had 132 00:05:01,830 --> 00:04:59,919 reduced the the antenna footprint on the 133 00:05:03,830 --> 00:05:01,840 spacecraft as you know 134 00:05:05,590 --> 00:05:03,840 you've seen the the iconic photo looking 135 00:05:08,230 --> 00:05:05,600 out of the blister of the soyuz as they 136 00:05:10,230 --> 00:05:08,240 approach the the iss and you can see an 137 00:05:12,629 --> 00:05:10,240 antenna that's rotating in the field of 138 00:05:14,790 --> 00:05:12,639 view that is a coors antenna that is no 139 00:05:16,870 --> 00:05:14,800 longer needed it was very complicated 140 00:05:19,189 --> 00:05:16,880 mechanically and also it had to be 141 00:05:20,629 --> 00:05:19,199 retracted prior to docking with the 142 00:05:22,790 --> 00:05:20,639 space station so that it didn't come in 143 00:05:24,710 --> 00:05:22,800 contact with station structure the new 144 00:05:27,110 --> 00:05:24,720 coors allows them to put a small phased 145 00:05:29,110 --> 00:05:27,120 array antenna on a fixed bracket that 146 00:05:30,870 --> 00:05:29,120 doesn't have to be retracted it weighs 147 00:05:33,590 --> 00:05:30,880 less uses less power it's much less 148 00:05:35,670 --> 00:05:33,600 complicated also you might recollect a 149 00:05:38,230 --> 00:05:35,680 boom on the aft end of the spacecraft 150 00:05:39,990 --> 00:05:38,240 that had two coors antennas that boom 151 00:05:41,749 --> 00:05:40,000 has been removed and the antenna has 152 00:05:43,830 --> 00:05:41,759 been placed on fixed locations on the 153 00:05:46,070 --> 00:05:43,840 spacecraft body so that simplifies the 154 00:05:48,230 --> 00:05:46,080 spacecraft and reduces weight all in all 155 00:05:50,870 --> 00:05:48,240 the the coors modifications 156 00:05:53,590 --> 00:05:50,880 reduced the weight of the the cool 157 00:05:57,029 --> 00:05:53,600 system by about 25 kilograms and takes 158 00:05:59,749 --> 00:05:57,039 about 30 less volume and it uses about 159 00:06:01,510 --> 00:05:59,759 24 less power so plus is all the way 160 00:06:02,710 --> 00:06:01,520 around 161 00:06:04,950 --> 00:06:02,720 another thing that they did to this 162 00:06:07,430 --> 00:06:04,960 spacecraft is change the 163 00:06:09,909 --> 00:06:07,440 approach and attitude control thrusters 164 00:06:11,909 --> 00:06:09,919 which in russian we call the depeo 165 00:06:14,790 --> 00:06:11,919 thrusters that are used to maneuver the 166 00:06:16,870 --> 00:06:14,800 spacecraft and change its orientation 167 00:06:18,870 --> 00:06:16,880 the previous depaol thrusters there were 168 00:06:21,270 --> 00:06:18,880 28 of them 16 of them were large 169 00:06:23,830 --> 00:06:21,280 thrusters of about 13 kilograms of 170 00:06:26,070 --> 00:06:23,840 thrust and 12 of them were small 171 00:06:29,029 --> 00:06:26,080 thrusters about 3 kilograms in thrust 172 00:06:31,189 --> 00:06:29,039 the new configuration uses 28 all large 173 00:06:33,830 --> 00:06:31,199 thrusters and it provides a lot of 174 00:06:35,990 --> 00:06:33,840 redundancy now by by 175 00:06:38,070 --> 00:06:36,000 uh 14 pairs of thrusters around the 176 00:06:40,309 --> 00:06:38,080 spacecraft so that there's a redundant 177 00:06:42,070 --> 00:06:40,319 thruster for every other thruster and 178 00:06:44,870 --> 00:06:42,080 they're operated on separate completely 179 00:06:46,870 --> 00:06:44,880 redundant manifolds for propellant so if 180 00:06:48,710 --> 00:06:46,880 one thruster fails the other thruster 181 00:06:51,510 --> 00:06:48,720 immediately in its pair immediately 182 00:06:53,909 --> 00:06:51,520 picks up and assumes control you recall 183 00:06:55,589 --> 00:06:53,919 in december when the 45 soyuz approached 184 00:06:57,670 --> 00:06:55,599 and they had a false indication of a 185 00:06:59,909 --> 00:06:57,680 thruster failing that required the crew 186 00:07:01,749 --> 00:06:59,919 members to manually take over and dock 187 00:07:03,189 --> 00:07:01,759 to the space station with the new 188 00:07:04,710 --> 00:07:03,199 thruster configuration that would not 189 00:07:06,950 --> 00:07:04,720 have been a problem a threat failure of 190 00:07:09,029 --> 00:07:06,960 one thruster just transitions to the 191 00:07:10,710 --> 00:07:09,039 thruster on the backup manifold 192 00:07:12,710 --> 00:07:10,720 the other advantage of the new thruster 193 00:07:15,029 --> 00:07:12,720 configuration is that on the aft end of 194 00:07:18,230 --> 00:07:15,039 the spacecraft there are eight thrusters 195 00:07:20,550 --> 00:07:18,240 instead of four so if during say a 196 00:07:23,189 --> 00:07:20,560 deorbit burn for example if the main 197 00:07:25,430 --> 00:07:23,199 engine were to fail now you have four 198 00:07:27,670 --> 00:07:25,440 large thrusters to be able to perform 199 00:07:29,350 --> 00:07:27,680 your deorbit burn instead of only four 200 00:07:31,189 --> 00:07:29,360 and so that provides additional level of 201 00:07:33,110 --> 00:07:31,199 redundancy as well 202 00:07:34,390 --> 00:07:33,120 how have all these modifications been 203 00:07:36,469 --> 00:07:34,400 tested mark 204 00:07:38,309 --> 00:07:36,479 well the testing has been comprehensive 205 00:07:41,189 --> 00:07:38,319 and extensive most or many of the 206 00:07:43,589 --> 00:07:41,199 modifications have already flown 207 00:07:46,230 --> 00:07:43,599 on previous versions of the soyuz even 208 00:07:48,070 --> 00:07:46,240 though they were tmam vehicles they one 209 00:07:50,629 --> 00:07:48,080 by one implemented some of the 210 00:07:52,710 --> 00:07:50,639 modifications they tested the redundant 211 00:07:54,309 --> 00:07:52,720 drive motors on the docking system they 212 00:07:56,070 --> 00:07:54,319 tested the core system so they've been 213 00:07:58,230 --> 00:07:56,080 tested on both progress and soyuz 214 00:08:00,469 --> 00:07:58,240 vehicles and then finally the last two 215 00:08:02,550 --> 00:08:00,479 progresses 62.63p 216 00:08:05,510 --> 00:08:02,560 have included all of the modifications 217 00:08:07,270 --> 00:08:05,520 comprehensively so that they'll have two 218 00:08:09,830 --> 00:08:07,280 positive flights and positive test 219 00:08:11,510 --> 00:08:09,840 results on progress vehicles giving them 220 00:08:12,950 --> 00:08:11,520 great confidence that the soyuz will be 221 00:08:15,029 --> 00:08:12,960 fine 222 00:08:17,510 --> 00:08:15,039 this launch will send kate rubins and 223 00:08:19,670 --> 00:08:17,520 her crewmates on a deliberate two-day 224 00:08:21,430 --> 00:08:19,680 rendezvous instead of the more common 225 00:08:23,189 --> 00:08:21,440 four-orbit six-hour rendezvous that 226 00:08:24,070 --> 00:08:23,199 we've become accustomed to 227 00:08:26,070 --> 00:08:24,080 why 228 00:08:28,230 --> 00:08:26,080 well the main reason for going to a 34 229 00:08:30,469 --> 00:08:28,240 orbit rendezvous on this flight is to 230 00:08:32,790 --> 00:08:30,479 provide additional time to test the new 231 00:08:35,110 --> 00:08:32,800 systems going to 34 orbit gives them 232 00:08:37,750 --> 00:08:35,120 lots of time to test the new unified or 233 00:08:39,509 --> 00:08:37,760 integrated command and telemetry system 234 00:08:40,949 --> 00:08:39,519 it gives them a chance to do some flying 235 00:08:43,670 --> 00:08:40,959 quality assessments with the new 236 00:08:45,750 --> 00:08:43,680 thruster configuration and it gives them 237 00:08:47,750 --> 00:08:45,760 a chance to test communications using 238 00:08:49,670 --> 00:08:47,760 the new luch satellites as well as the