1 00:00:07,760 --> 00:00:05,230 [Music] 2 00:00:09,650 --> 00:00:07,770 hi I'm Marvin Barnes and I'm the 3 00:00:15,350 --> 00:00:09,660 principal investigator for this SIF 4 00:00:17,150 --> 00:00:15,360 project together we're developing 5 00:00:20,150 --> 00:00:17,160 nuclear fuel for nuclear rocket engines 6 00:00:23,090 --> 00:00:20,160 in FY 18 we were awarded center 7 00:00:25,910 --> 00:00:23,100 innovation funding to fabricate test and 8 00:00:27,080 --> 00:00:25,920 characterize nuclear fuel samples this 9 00:00:28,400 --> 00:00:27,090 work is being performed as a 10 00:00:30,380 --> 00:00:28,410 collaboration with the University of 11 00:00:32,630 --> 00:00:30,390 Tennessee where advanced 12 00:00:34,880 --> 00:00:32,640 characterization is taking place in 13 00:00:37,220 --> 00:00:34,890 house we're doing the fabrication and 14 00:00:38,720 --> 00:00:37,230 the testing of these fuel materials my 15 00:00:40,520 --> 00:00:38,730 name is taylor Duffin I'm a graduate 16 00:00:42,740 --> 00:00:40,530 student from University of Tennessee in 17 00:00:45,529 --> 00:00:42,750 Knoxville our sip project supports 18 00:00:48,200 --> 00:00:45,539 nuclear thermal propulsion NTP is an 19 00:00:51,290 --> 00:00:48,210 in-space propulsion technology which is 20 00:00:54,470 --> 00:00:51,300 useful for supporting crewed missions 21 00:00:56,630 --> 00:00:54,480 beyond low-earth orbit to Mars if we use 22 00:00:59,209 --> 00:00:56,640 NTP we can reduce our travel times and 23 00:01:01,340 --> 00:00:59,219 harmful effects to our astronauts the 24 00:01:04,009 --> 00:01:01,350 fuel for NTP is one of the major 25 00:01:06,170 --> 00:01:04,019 limiting factors in this SIF we're 26 00:01:08,359 --> 00:01:06,180 developing a molybdenum sermon or 27 00:01:10,880 --> 00:01:08,369 ceramic metallic fuels as an alternative 28 00:01:12,649 --> 00:01:10,890 to tungsten these molybdenum fuels will 29 00:01:14,600 --> 00:01:12,659 be more affordable than tungsten based 30 00:01:17,330 --> 00:01:14,610 one the main objective for this project 31 00:01:19,010 --> 00:01:17,340 is to identify the maximum use 32 00:01:20,960 --> 00:01:19,020 temperature for molybdenum sarmento 33 00:01:22,910 --> 00:01:20,970 fuels in both thermal cycling and 34 00:01:24,620 --> 00:01:22,920 steady-state conditions in the 35 00:01:28,340 --> 00:01:24,630 molybdenum Cir matte powder blending 36 00:01:30,580 --> 00:01:28,350 process we have molybdenum ceramic fuel 37 00:01:33,499 --> 00:01:30,590 element and the binder mixed together 38 00:01:36,560 --> 00:01:33,509 and the binder is there to hold 39 00:01:39,020 --> 00:01:36,570 everything together nicely then they are 40 00:01:41,480 --> 00:01:39,030 mixed in the turbulent heated and 41 00:01:46,130 --> 00:01:41,490 stirred to produce an even coating this 42 00:01:48,020 --> 00:01:46,140 allows for optimal fuel performance we 43 00:01:51,710 --> 00:01:48,030 turn our powders into solid samples 44 00:01:53,569 --> 00:01:51,720 using spark plasma sintering we are 45 00:01:56,120 --> 00:01:53,579 optimizing time temperature and pressure 46 00:01:59,660 --> 00:01:56,130 to make fully dense samples with the 47 00:02:02,030 --> 00:01:59,670 best micro structures we perform high 48 00:02:04,850 --> 00:02:02,040 temperature testing on our samples in C 49 00:02:06,830 --> 00:02:04,860 feet up to 2500 Kelvin and low flowing 50 00:02:09,499 --> 00:02:06,840 hydrogen to simulate the conditions in 51 00:02:11,240 --> 00:02:09,509 the nuclear rocket engine we observe the 52 00:02:13,050 --> 00:02:11,250 mass loss to the sample and then 53 00:02:15,120 --> 00:02:13,060 characterize the 54 00:02:17,910 --> 00:02:15,130 Appl microstrain jizz that have occurred 55 00:02:20,070 --> 00:02:17,920 by advanced microscopy through this 56 00:02:22,260 --> 00:02:20,080 project we are able to produce high 57 00:02:25,140 --> 00:02:22,270 density molybdenum sermonette fuels with 58 00:02:27,170 --> 00:02:25,150 desirable micro structures we will be 59 00:02:30,150 --> 00:02:27,180 recommending maximum use temperatures 60 00:02:32,280 --> 00:02:30,160 derived from testing data thank you for 61 00:02:34,020 --> 00:02:32,290 the funding we hope that the technology 62 00:02:36,660 --> 00:02:34,030 developed through the SIF project will