1 00:00:10,400 --> 00:00:08,720 satellites have a have a common problem 2 00:00:11,629 --> 00:00:10,410 and that is they're always power starved 3 00:00:13,580 --> 00:00:11,639 no matter where you are there's not 4 00:00:16,450 --> 00:00:13,590 enough power and conventional solar 5 00:00:18,980 --> 00:00:16,460 power comes from rigid deployable arrays 6 00:00:21,200 --> 00:00:18,990 typically with cover glass they're 7 00:00:23,570 --> 00:00:21,210 somewhat fragile easily damaged during 8 00:00:25,820 --> 00:00:23,580 packaging and it's difficult to get a 9 00:00:27,320 --> 00:00:25,830 lot of power in a small spacecraft which 10 00:00:29,630 --> 00:00:27,330 is the current generation of cube SATs 11 00:00:30,980 --> 00:00:29,640 and ultra small spacecraft what we're 12 00:00:33,860 --> 00:00:30,990 doing in this test is we're 13 00:00:36,560 --> 00:00:33,870 demonstrating the ability to take next 14 00:00:38,900 --> 00:00:36,570 generation very flexible solar arrays 15 00:00:41,750 --> 00:00:38,910 fold them package them into a very small 16 00:00:44,090 --> 00:00:41,760 volume and deploy them once they're in 17 00:00:45,890 --> 00:00:44,100 space so that you can get a large 18 00:00:54,670 --> 00:00:45,900 surface area and generate a lot of power 19 00:00:58,939 --> 00:00:57,350 the way this all got started was we were 20 00:01:02,299 --> 00:00:58,949 working with several companies on very 21 00:01:03,740 --> 00:01:02,309 thin film lightweight solar cells these 22 00:01:04,850 --> 00:01:03,750 are very different than the solar cells 23 00:01:07,460 --> 00:01:04,860 that are used in space applications 24 00:01:09,740 --> 00:01:07,470 today and they they're very flexible 25 00:01:12,290 --> 00:01:09,750 they're very light and they're mountable 26 00:01:15,080 --> 00:01:12,300 on on a variety of substrates including 27 00:01:16,280 --> 00:01:15,090 aluminum or captain and we were thinking 28 00:01:18,320 --> 00:01:16,290 about structures that we can mount them 29 00:01:19,670 --> 00:01:18,330 on and we realized that inflatable 30 00:01:21,530 --> 00:01:19,680 structures were were the perfect 31 00:01:24,680 --> 00:01:21,540 mounting structures for those and that 32 00:01:26,270 --> 00:01:24,690 they gave us a very rigid structure that 33 00:01:29,600 --> 00:01:26,280 would hold the lightweight array and 34 00:01:31,219 --> 00:01:29,610 would also provide very small storage 35 00:01:37,660 --> 00:01:31,229 volume for the array that you end up 36 00:01:43,210 --> 00:01:39,820 the unit you see who came from a concept 37 00:01:46,210 --> 00:01:43,220 study that we did for a micro set that 38 00:01:48,400 --> 00:01:46,220 would implement a telescope application 39 00:01:50,590 --> 00:01:48,410 and so we took the concept design that 40 00:01:51,610 --> 00:01:50,600 we had and actually built the test 41 00:01:54,400 --> 00:01:51,620 article out of it 42 00:01:56,080 --> 00:01:54,410 the silver substrate pieces that you see 43 00:01:57,850 --> 00:01:56,090 aren't print of the solar arrays but we 44 00:02:00,250 --> 00:01:57,860 had one actual solar cell that we 45 00:02:02,410 --> 00:02:00,260 attached to the pedal instrumented and 46 00:02:03,969 --> 00:02:02,420 we did flash tests of it in the 47 00:02:05,770 --> 00:02:03,979 beginning and we wrapped it up for 48 00:02:07,300 --> 00:02:05,780 deployment now we've done the deployment 49 00:02:09,219 --> 00:02:07,310 and you know do another test to assure 50 00:02:16,620 --> 00:02:09,229 that the deployment hasn't damaged it 51 00:02:20,400 --> 00:02:18,480 there are a lot of applications for this 52 00:02:22,740 --> 00:02:20,410 technology we envision that you could 53 00:02:25,170 --> 00:02:22,750 use this inflatable or deployables solar 54 00:02:27,360 --> 00:02:25,180 array system everything from cube SATs 55 00:02:29,520 --> 00:02:27,370 which are was a very small 10 centimeter 56 00:02:31,560 --> 00:02:29,530 by 10 centimeter spacecraft which are 57 00:02:33,510 --> 00:02:31,570 typically very very power limited 58 00:02:36,030 --> 00:02:33,520 something like this could be packaged in 59 00:02:38,400 --> 00:02:36,040 about 1/3 of the volume and inflate to 60 00:02:40,800 --> 00:02:38,410 something this size providing unheard of 61 00:02:43,020 --> 00:02:40,810 power for small SATs primarily in 62 00:02:44,520 --> 00:02:43,030 low-earth orbit you could also take this 63 00:02:47,160 --> 00:02:44,530 technology and use it for human 64 00:02:49,560 --> 00:02:47,170 exploration in deep space and deploy 65 00:02:52,380 --> 00:02:49,570 incredibly large thanks size of this 66 00:03:09,020 --> 00:02:52,390 room or bigger arrays packaged into 67 00:03:14,070 --> 00:03:12,090 the next steps for the technology are to 68 00:03:16,470 --> 00:03:14,080 take this demonstration which we believe 69 00:03:19,559 --> 00:03:16,480 is shown of the viability of this at 70 00:03:21,570 --> 00:03:19,569 technology readiness level 4 and start