1 00:00:01,179 --> 00:00:03,290 Developing next generation , research 2 00:00:03,290 --> 00:00:04,960 and technology , facilitating 3 00:00:04,969 --> 00:00:07,136 connections between a FRL industry and 4 00:00:07,136 --> 00:00:09,358 academia . Unlocking innovation through 5 00:00:09,358 --> 00:00:11,413 a culture of collaboration . This is 6 00:00:11,413 --> 00:00:13,569 the A FRL Regional Network Midwest . 7 00:00:17,399 --> 00:00:19,621 My background is in energetic materials 8 00:00:19,621 --> 00:00:22,760 in solid propellant , solid fuels . And 9 00:00:22,770 --> 00:00:24,659 in this project , we're trying to 10 00:00:24,659 --> 00:00:27,620 integrate uh solid fuels into uh 11 00:00:27,629 --> 00:00:30,129 rotating detonation engines in solid 12 00:00:30,139 --> 00:00:32,439 fuels . Why we're interested in that is 13 00:00:32,450 --> 00:00:35,549 because they're much easier to store , 14 00:00:35,939 --> 00:00:38,130 they don't leak . So if there's a 15 00:00:38,139 --> 00:00:41,909 puncture in the device , you're not 16 00:00:41,919 --> 00:00:44,549 going to have a fire hazard with that 17 00:00:44,810 --> 00:00:46,754 potentially , it could have higher 18 00:00:46,754 --> 00:00:49,950 energy density . But the challenge of 19 00:00:49,959 --> 00:00:53,590 bringing in a solid fuel into the RD is 20 00:00:53,599 --> 00:00:56,509 how do we integrate it in ? How do we 21 00:00:56,520 --> 00:01:00,299 go from a solid fuel to a gaseous fuel 22 00:01:00,310 --> 00:01:03,770 that the RD can operate with ? So 23 00:01:03,779 --> 00:01:06,739 that's a big focus of this project is 24 00:01:06,889 --> 00:01:10,209 looking at fuels that can gasify on 25 00:01:10,220 --> 00:01:12,331 their own . So we don't have to bring 26 00:01:12,331 --> 00:01:15,500 in energy to turn that fuel into gas , 27 00:01:15,529 --> 00:01:18,059 but they burn , they propagate and 28 00:01:18,069 --> 00:01:20,580 produce gas that can be fed into the 29 00:01:20,589 --> 00:01:22,769 rotating detonation engine . Some of 30 00:01:22,779 --> 00:01:25,001 the advantages of a rotating detonation 31 00:01:25,001 --> 00:01:26,835 engine include increased thermal 32 00:01:26,835 --> 00:01:28,446 efficiency due to the higher 33 00:01:28,446 --> 00:01:30,557 temperatures and pressures that occur 34 00:01:30,557 --> 00:01:33,209 during a detonation . In the video 35 00:01:33,220 --> 00:01:34,942 shown here , for example , the 36 00:01:34,942 --> 00:01:36,942 detonation wave is propagating at a 37 00:01:36,942 --> 00:01:40,000 speed of over 1500 m per second , which 38 00:01:40,010 --> 00:01:43,849 is over 3000 MPH . This is up to 100 39 00:01:43,860 --> 00:01:45,970 times faster than the flame in a 40 00:01:45,980 --> 00:01:48,639 typical engine which leads to increased 41 00:01:48,650 --> 00:01:50,839 power density so that the combustion 42 00:01:50,860 --> 00:01:53,550 can be made much more compact , simple 43 00:01:53,559 --> 00:01:56,110 and lightweight than a normal combust , 44 00:01:56,370 --> 00:01:58,519 which reduces the overall fuel 45 00:01:58,529 --> 00:02:00,569 consumption . So the goal of the 46 00:02:00,580 --> 00:02:02,610 research at Purdue University is to 47 00:02:02,620 --> 00:02:04,790 investigate the types of solid 48 00:02:04,800 --> 00:02:06,689 propellants that can be used in a 49 00:02:06,689 --> 00:02:09,050 rotating detonation engine as well as 50 00:02:09,059 --> 00:02:11,170 the systems that would be required to 51 00:02:11,170 --> 00:02:13,170 incorporate those solid propellants 52 00:02:13,170 --> 00:02:15,410 effectively in an operating rotating 53 00:02:15,419 --> 00:02:17,586 detonation engine . For this project , 54 00:02:17,586 --> 00:02:19,752 we're looking for solid fuel with some 55 00:02:19,752 --> 00:02:21,975 pretty unique characteristics . First , 56 00:02:21,975 --> 00:02:23,752 we wanted it to be able to self 57 00:02:23,820 --> 00:02:26,350 defecate in a non oxygen atmosphere and 58 00:02:26,360 --> 00:02:28,582 that's pretty important for how we will 59 00:02:28,582 --> 00:02:31,050 get it to actually work in an RD . Um 60 00:02:31,059 --> 00:02:33,149 We also wanted to produce very fuel 61 00:02:33,160 --> 00:02:35,580 rich exhaust products , uh ones that 62 00:02:35,589 --> 00:02:38,259 are hopefully very de like hydrogen gas . 63 00:02:38,789 --> 00:02:41,011 Um And ideally , this is something that 64 00:02:41,011 --> 00:02:43,820 we want to be able to produce in house . 65 00:02:43,830 --> 00:02:45,886 Um That way we can kind of fine tune 66 00:02:45,886 --> 00:02:48,199 the formulation or add in any type of 67 00:02:48,210 --> 00:02:50,432 uh energetic additives as well . One of 68 00:02:50,432 --> 00:02:52,543 the first things that we did for this 69 00:02:52,543 --> 00:02:54,488 project was um essentially using a 70 00:02:54,488 --> 00:02:57,449 synthetic mixture to simulate what we 71 00:02:57,460 --> 00:03:00,070 think our solid fuel will produce in 72 00:03:00,080 --> 00:03:03,880 the RD . So to do that , we use NASA CE 73 00:03:03,889 --> 00:03:06,009 A which is a chemical equilibrium of 74 00:03:06,020 --> 00:03:09,009 applications code in order to simulate 75 00:03:09,020 --> 00:03:11,899 the propellant burning . And then we 76 00:03:11,910 --> 00:03:14,610 were able to take that and take the , 77 00:03:15,059 --> 00:03:17,759 the constituent gasses , mix them 78 00:03:17,770 --> 00:03:20,619 together and fire that in an RD . So 79 00:03:20,630 --> 00:03:22,797 that's one of something that one of my 80 00:03:22,797 --> 00:03:25,074 previous colleagues did here at Purdue . 81 00:03:25,074 --> 00:03:27,297 We have many RD that we're able to test 82 00:03:27,297 --> 00:03:30,169 with . Specifically , we have optically 83 00:03:30,179 --> 00:03:32,290 accessible ones , which is useful for 84 00:03:32,290 --> 00:03:34,512 us to visualize what's happening inside 85 00:03:34,512 --> 00:03:37,070 the RDE . And we use these in the solid 86 00:03:37,080 --> 00:03:39,929 fuel project to do our tests . So one 87 00:03:39,940 --> 00:03:42,107 of the next things that we did was use 88 00:03:42,107 --> 00:03:44,479 Raman spectroscopy to actually measure 89 00:03:44,490 --> 00:03:47,399 the products of our solid fuel NASA . 90 00:03:47,869 --> 00:03:51,839 Because any software , especially one 91 00:03:51,850 --> 00:03:54,460 that's kind of first order like NASA CE 92 00:03:54,470 --> 00:03:56,750 A is going to produce results that are 93 00:03:56,759 --> 00:03:59,220 not necessarily in line with reality . 94 00:03:59,649 --> 00:04:01,760 So using Ramus photocopy , we're able 95 00:04:01,760 --> 00:04:03,482 to very accurately measure the 96 00:04:03,490 --> 00:04:05,679 concentration of all the different 97 00:04:05,690 --> 00:04:09,000 species inside our solid fuel exhaust 98 00:04:09,009 --> 00:04:11,399 products . And that kind of helps us 99 00:04:11,410 --> 00:04:13,759 determine if we need to tweak the 100 00:04:13,770 --> 00:04:16,589 formulation as well as will give us a 101 00:04:16,600 --> 00:04:18,544 better understanding of I actually 102 00:04:18,544 --> 00:04:20,433 operate inside an RD . One of the 103 00:04:20,470 --> 00:04:22,081 things that we want to do is 104 00:04:22,081 --> 00:04:24,248 characterize how detain those products 105 00:04:24,248 --> 00:04:26,359 are . And so we use a detonation tube 106 00:04:26,359 --> 00:04:28,679 which is essentially a long acrylic 107 00:04:28,690 --> 00:04:30,912 tube that we're able to image with high 108 00:04:30,912 --> 00:04:33,023 speed cameras to actually measure how 109 00:04:33,023 --> 00:04:35,246 fast those exhaust products are able to 110 00:04:35,246 --> 00:04:37,529 detonate . And in doing that , we're 111 00:04:37,540 --> 00:04:39,373 able to kind of give ourselves a 112 00:04:39,373 --> 00:04:41,540 benchmark for how well our formulation 113 00:04:41,540 --> 00:04:43,760 is doing . And that kind of is an 114 00:04:43,769 --> 00:04:45,713 important metric to understand how 115 00:04:45,720 --> 00:04:47,831 we'll actually operate inside of A RD 116 00:04:47,831 --> 00:04:50,200 once we get to that point . So our next 117 00:04:50,209 --> 00:04:52,049 steps in the near term future is 118 00:04:52,059 --> 00:04:54,540 scaling up our production of the solid 119 00:04:54,549 --> 00:04:56,739 fuel that's going to allow us to do 120 00:04:56,750 --> 00:04:58,917 larger scale tests as well as actually 121 00:04:58,917 --> 00:05:01,790 integrate the solid fuel into the RD . 122 00:05:02,250 --> 00:05:04,410 Um We're also been looking at various 123 00:05:04,420 --> 00:05:06,779 additives that we can add to that solid 124 00:05:06,790 --> 00:05:09,429 fuel formulation to produce exhaust 125 00:05:09,440 --> 00:05:11,790 products that are more tailored to the 126 00:05:11,799 --> 00:05:14,269 specific use case . Some of the 127 00:05:14,279 --> 00:05:16,279 experimental setups that we've been 128 00:05:16,279 --> 00:05:18,112 updating , we have a new raw and 129 00:05:18,112 --> 00:05:20,057 spectroscopy setup that's going to 130 00:05:20,057 --> 00:05:22,010 allow us to measure the solid fuel 131 00:05:22,019 --> 00:05:24,470 exhaust products in a more realistic 132 00:05:24,480 --> 00:05:26,690 environment . And that's going to give 133 00:05:26,700 --> 00:05:28,422 us a better idea of the actual 134 00:05:28,422 --> 00:05:30,422 formulation that we're working with 135 00:05:30,422 --> 00:05:32,690 inside the RD . And then we also have a 136 00:05:32,700 --> 00:05:35,209 larger det tube . Um that's gonna kind 137 00:05:35,220 --> 00:05:37,442 of fix some of the issues that we first 138 00:05:37,442 --> 00:05:39,609 saw in the original setup and allow us 139 00:05:39,609 --> 00:05:41,831 to give , allow us to get more accurate 140 00:05:41,831 --> 00:05:43,942 measurements of the wave speed of our 141 00:05:43,942 --> 00:05:46,053 detonation . The idea to use uh solid 142 00:05:46,053 --> 00:05:48,220 propellants for rotating detonation is 143 00:05:48,220 --> 00:05:51,230 a fairly new one . So some of the 144 00:05:51,239 --> 00:05:53,730 innovative work that's been done uh at 145 00:05:53,799 --> 00:05:56,109 Purdue and a couple other places in the 146 00:05:56,119 --> 00:05:58,286 US is really cutting edge technology . 147 00:05:58,709 --> 00:06:01,769 So , um we've demonstrated burning uh 148 00:06:01,779 --> 00:06:05,179 propellants um and producing something 149 00:06:05,190 --> 00:06:07,357 that could then burn again in a , in a 150 00:06:07,357 --> 00:06:09,412 rotating detonation engine . So that 151 00:06:09,412 --> 00:06:11,634 proof of concept is really key to being 152 00:06:11,634 --> 00:06:13,857 able to turn on , you know , additional 153 00:06:13,857 --> 00:06:16,570 funds to , to , you know , do a more 154 00:06:16,579 --> 00:06:20,420 substantive effort in maturing this 155 00:06:20,429 --> 00:06:22,260 technology for , for an actual 156 00:06:22,269 --> 00:06:24,859 application . Um There's a lot of work 157 00:06:24,869 --> 00:06:27,250 been done with liquids , but rotating 158 00:06:27,260 --> 00:06:29,799 detonation with solid fuel is is pretty 159 00:06:29,809 --> 00:06:33,000 new , new game . It's a very high 160 00:06:33,079 --> 00:06:35,869 interest technology across department 161 00:06:35,880 --> 00:06:38,190 of defense . So uh it's a very 162 00:06:38,200 --> 00:06:40,390 important technology for the war 163 00:06:40,399 --> 00:06:40,890 fighter .