1 00:00:00,000 --> 00:00:10,376 Music and sound effects. 2 00:00:14,639 --> 00:00:16,344 atomic clocks are central to 3 00:00:16,379 --> 00:00:18,296 deep space navigation it's 4 00:00:18,331 --> 00:00:19,480 just that those clocks are 5 00:00:19,515 --> 00:00:21,448 on the ground. And so an 6 00:00:21,483 --> 00:00:24,280 atomic clock generates a signal 7 00:00:24,315 --> 00:00:25,689 and it is sent through the 8 00:00:25,724 --> 00:00:27,864 antennae on the ground to a 9 00:00:27,899 --> 00:00:29,672 spacecraft in deep space. And 10 00:00:29,707 --> 00:00:31,769 that signal is turned around 11 00:00:31,804 --> 00:00:33,241 and received back at the 12 00:00:33,276 --> 00:00:34,728 transmitting. And with that 13 00:00:34,763 --> 00:00:37,064 transmission of the signal 14 00:00:37,099 --> 00:00:38,152 we can do measurements of that 15 00:00:38,187 --> 00:00:39,960 signal. You know how the 16 00:00:39,995 --> 00:00:41,593 doppler shift on the signal 17 00:00:41,628 --> 00:00:43,752 is how we can know how fast 18 00:00:43,787 --> 00:00:45,593 the spacecraft is moving and 19 00:00:45,628 --> 00:00:47,112 how long that signal takes 20 00:00:47,147 --> 00:00:48,792 is a measure of how far that 21 00:00:48,827 --> 00:00:51,064 spacecraft is. So the deep 22 00:00:51,099 --> 00:00:52,792 space atomic clock can change 23 00:00:52,827 --> 00:00:54,616 that paradigm. It can originate 24 00:00:54,651 --> 00:00:56,152 the signal at the earth 25 00:00:56,187 --> 00:00:57,480 and it can end at the 26 00:00:57,515 --> 00:00:59,368 spacecraft. Its good enough, that 27 00:00:59,403 --> 00:01:00,840 small clock that we are 28 00:01:00,875 --> 00:01:02,440 building is as stable and 29 00:01:02,475 --> 00:01:04,664 accurate as the ground clock 30 00:01:04,699 --> 00:01:07,465 that originated the signal. We 31 00:01:07,500 --> 00:01:08,985 get to utilize some of the 32 00:01:09,020 --> 00:01:10,455 efficiencies that the deep space 33 00:01:10,490 --> 00:01:11,736 tracking network has to 34 00:01:11,771 --> 00:01:13,368 offer today. The DSN supports 35 00:01:13,403 --> 00:01:16,072 more downlink than it does 36 00:01:16,107 --> 00:01:17,801 uplink and so at places 37 00:01:17,836 --> 00:01:19,640 like Mars where we have a 38 00:01:19,675 --> 00:01:21,096 number of spacecraft that are 39 00:01:21,131 --> 00:01:22,184 competing for two-way tracking 40 00:01:22,219 --> 00:01:23,801 time... you don't have to 41 00:01:23,836 --> 00:01:25,689 do that anymore. What does 42 00:01:25,724 --> 00:01:27,033 that do for us? well what we 43 00:01:27,068 --> 00:01:28,792 have found with a 2 times 44 00:01:28,827 --> 00:01:30,264 improvement in our tracking 45 00:01:30,299 --> 00:01:31,880 data for a Mars orbiter, the 46 00:01:31,915 --> 00:01:33,944 orbit information that we get 47 00:01:33,979 --> 00:01:35,608 is improved upon by a factor 48 00:01:35,643 --> 00:01:38,248 of five. One of the things 49 00:01:38,283 --> 00:01:39,656 we are envisioning at Mars 50 00:01:39,691 --> 00:01:42,457 is landing a pin-point lander, 51 00:01:42,492 --> 00:01:43,960 one that can land to a 52 00:01:43,995 --> 00:01:45,353 very precise location (beep 53 00:01:45,388 --> 00:01:46,855 sounds) on the surface of Mars. 54 00:01:46,890 --> 00:01:48,136 there's a lot of steps into 55 00:01:48,171 --> 00:01:49,464 making that happen. One of 56 00:01:49,499 --> 00:01:51,160 which is entering the top 57 00:01:51,195 --> 00:01:52,521 of the atmosphere and taking 58 00:01:52,556 --> 00:01:54,760 your entry state knowledge 59 00:01:54,795 --> 00:01:56,920 and onboard flying a 60 00:01:56,955 --> 00:01:58,361 trajectory with that entry state 61 00:01:58,396 --> 00:01:59,673 knowledge. We way in which we 62 00:01:59,708 --> 00:02:00,857 upload that navigation state 63 00:02:00,892 --> 00:02:02,329 today is that we do all the 64 00:02:02,364 --> 00:02:03,753 processing on the ground in about 65 00:02:03,788 --> 00:02:05,592 six or so hours and before 66 00:02:05,627 --> 00:02:07,992 entry we upload a final nav state 67 00:02:08,027 --> 00:02:09,880 to the vehicle. Well you can 68 00:02:09,915 --> 00:02:11,833 imagine after six hours of flight 69 00:02:11,868 --> 00:02:13,352 that solutions is little stale 70 00:02:13,387 --> 00:02:14,873 when you get to the top of the 71 00:02:14,908 --> 00:02:16,664 atmosphere. Well with DSAC with 72 00:02:16,699 --> 00:02:18,696 the measurement happening onboard 73 00:02:18,731 --> 00:02:20,839 you don't have to suffer that six 74 00:02:20,874 --> 00:02:22,776 hour delay. You can be computing 75 00:02:22,811 --> 00:02:24,472 onboard in real time. And what 76 00:02:24,507 --> 00:02:26,792 that does is where the six hour 77 00:02:26,827 --> 00:02:30,169 solution is in error by a few 78 00:02:30,204 --> 00:02:32,312 kilometers, this solution that's 79 00:02:32,347 --> 00:02:33,928 onboard is only off by a handful 80 00:02:33,963 --> 00:02:36,073 meters. that has a real benefit 81 00:02:36,108 --> 00:02:37,769 to decreasing the amount of 82 00:02:37,804 --> 00:02:39,848 propellant you have to carry to then 83 00:02:39,883 --> 00:02:41,816 later fly out the errors you had 84 00:02:41,851 --> 00:02:43,897 when you didn't know where you 85 00:02:43,932 --> 00:02:46,248 were at when you originally were 86 00:02:46,283 --> 00:02:47,176 at the top of the atmosphere.So 87 00:02:47,211 --> 00:02:48,440 that's gonna open up new ways, 88 00:02:48,475 --> 00:02:50,104 new science we are going to be 89 00:02:50,139 --> 00:02:51,336 able to do. In fact it's going 90 00:02:51,371 --> 00:02:52,568 to improve the gravity science 91 00:02:52,603 --> 00:02:54,280 we are going to be able to do 92 00:02:54,315 --> 00:02:55,993 at Mars today. An example of 93 00:02:56,028 --> 00:02:58,104 gravity science improvement that 94 00:02:58,139 --> 00:03:00,248 the clock enables further out is 95 00:03:00,283 --> 00:03:03,112 NASA is envisioning going to 96 00:03:03,147 --> 00:03:05,176 Europa; an moon around jupiter. And 97 00:03:05,211 --> 00:03:08,873 to be able to do the measurement, 98 00:03:08,908 --> 00:03:10,824 the gravity science measurement 99 00:03:10,859 --> 00:03:13,849 that NASA is planning. They're 100 00:03:13,884 --> 00:03:15,368 going to do it, one approach 101 00:03:15,403 --> 00:03:18,088 is a flyby mission. So they will 102 00:03:18,123 --> 00:03:19,896 fly by Europa with a four hour 103 00:03:19,931 --> 00:03:21,960 tracking pass, and then have a 104 00:03:21,995 --> 00:03:24,680 thirty day orbit around Europa, 105 00:03:24,715 --> 00:03:25,673 and then come back again for 106 00:03:25,708 --> 00:03:26,889 another flyby. And do a sequence 107 00:03:26,924 --> 00:03:29,753 of thirty or so of these flybys. 108 00:03:29,788 --> 00:03:32,072 Well if we have the atomic clock 109 00:03:32,107 --> 00:03:34,840 on a downlink signal from that 110 00:03:34,875 --> 00:03:36,408 flyby and it's received at the 111 00:03:36,443 --> 00:03:39,385 earth we can do it at Ka band. 112 00:03:39,420 --> 00:03:41,145 and the benefit of going to Ka 113 00:03:41,180 --> 00:03:43,048 band isn't so much that it has 114 00:03:43,083 --> 00:03:44,361 to deal with we can increase the 115 00:03:44,396 --> 00:03:46,473 bandwidth but what it does do 116 00:03:46,508 --> 00:03:48,887 is that it improves the accuracy 117 00:03:48,922 --> 00:03:50,248 of the measurement that we are 118 00:03:50,283 --> 00:03:51,528 taking, and it improves it by an 119 00:03:51,563 --> 00:03:52,920 order of magnitude and that is 120 00:03:52,955 --> 00:03:54,616 fundemental. Its that improvement 121 00:03:54,651 --> 00:03:57,864 in the data quality that will 122 00:03:57,899 --> 00:03:59,689 allow us to determine the gravity 123 00:03:59,724 --> 00:04:03,513 well enough. If decisions need 124 00:04:03,548 --> 00:04:05,400 to be made in real time, the