1 00:00:01,001 --> 00:00:07,513 Music 2 00:00:07,548 --> 00:00:09,120 What we’re building is the MSA 3 00:00:09,155 --> 00:00:10,896 Diaphragm, and what this is, is 4 00:00:10,931 --> 00:00:12,911 it fits between the propellant 5 00:00:12,946 --> 00:00:15,151 stage of the rocket and the 6 00:00:15,186 --> 00:00:17,111 Orion capsule. This is a very 7 00:00:17,146 --> 00:00:19,295 important barrier that we need 8 00:00:19,330 --> 00:00:20,664 to have on this rocket to keep 9 00:00:20,699 --> 00:00:22,888 the hazardous coming of the 10 00:00:22,923 --> 00:00:24,640 propellant stage from getting up 11 00:00:24,675 --> 00:00:26,319 into the Orion capsule. 12 00:00:26,354 --> 00:00:27,856 The diaphragm is 100% composite 13 00:00:27,891 --> 00:00:30,951 structure, that is a fabric that 14 00:00:30,986 --> 00:00:33,566 is a carbon fiber fabric with epoxy. 15 00:00:33,601 --> 00:00:36,648 And when this is all put together 16 00:00:36,683 --> 00:00:38,560 it makes for a very strong, very 17 00:00:38,595 --> 00:00:40,175 light weight structure, and 18 00:00:40,210 --> 00:00:42,808 that’s key for space flight. 19 00:00:42,843 --> 00:00:44,520 Well this is the flight diaphragm 20 00:00:44,555 --> 00:00:45,696 that will actually fly in the 21 00:00:45,731 --> 00:00:47,575 first Orion, the EFT1 flight test. 22 00:00:47,610 --> 00:00:49,271 And with any new structure we 23 00:00:49,306 --> 00:00:50,974 have to proof test it to make 24 00:00:51,009 --> 00:00:52,231 sure it can withstand the 25 00:00:52,266 --> 00:00:53,608 structural capability of the 26 00:00:53,643 --> 00:00:55,737 flight loads, which also includes 27 00:00:55,772 --> 00:00:57,504 thermal loads, inertial loads. 28 00:00:57,539 --> 00:00:59,592 So the main design drivers for 29 00:00:59,627 --> 00:01:01,736 the diaphragm were to handle 30 00:01:01,771 --> 00:01:04,376 launch loads which can be up 31 00:01:04,411 --> 00:01:05,815 to 5 Gs, and also a pressure 32 00:01:05,850 --> 00:01:09,095 difference between the propellant 33 00:01:09,130 --> 00:01:11,640 stage and the Orion capsule. 34 00:01:11,675 --> 00:01:13,936 And so that pressure difference 35 00:01:13,971 --> 00:01:15,584 is what we are testing here today. 36 00:01:15,619 --> 00:01:17,392 When you’re dealing with composites, 37 00:01:17,427 --> 00:01:19,096 it’s a very process sensitive 38 00:01:19,131 --> 00:01:21,359 material to use, and so every time 39 00:01:21,394 --> 00:01:22,679 that you use composites you 40 00:01:22,714 --> 00:01:24,575 really need to get acceptance 41 00:01:24,610 --> 00:01:27,039 from the engineering community 42 00:01:27,074 --> 00:01:31,144 about how to fabricate and test 43 00:01:31,179 --> 00:01:33,544 the composite that you are using. 44 00:01:33,579 --> 00:01:35,704 So that has been the most 45 00:01:35,739 --> 00:01:36,952 challenging thing I think is to 46 00:01:36,987 --> 00:01:38,944 really develop a road map that the 47 00:01:38,979 --> 00:01:41,023 engineering community can get 48 00:01:41,058 --> 00:01:43,943 buy-in to and to prove out that 49 00:01:43,978 --> 00:01:46,560 the design that we are making and 50 00:01:46,595 --> 00:01:47,825 that the analysis that we are 51 00:01:47,860 --> 00:01:49,448 showing is good; can be 52 00:01:49,483 --> 00:01:50,856 substantiated by tests. 53 00:01:50,891 --> 00:01:53,936 We actually installed tri-axial 54 00:01:53,971 --> 00:01:55,384 string gauges so measures any 55 00:01:55,419 --> 00:01:58,263 strain that the article sees and 56 00:01:58,298 --> 00:02:00,191 that way the test requester can 57 00:02:00,226 --> 00:02:01,912 watch the data in real-time as we 58 00:02:01,947 --> 00:02:03,775 are applying load, and make sure 59 00:02:03,810 --> 00:02:05,807 that it’s not exceeding any kind 60 00:02:05,842 --> 00:02:07,464 of strain that he predicted. 61 00:02:07,499 --> 00:02:09,912 There is a bench mark in using 62 00:02:09,947 --> 00:02:11,544 composites in this way. It’s the 63 00:02:11,579 --> 00:02:14,152 largest structure made entirely of 64 00:02:14,187 --> 00:02:16,015 composite that NASA has endorsed 65 00:02:16,050 --> 00:02:17,535 to be put on a space craft. 66 00:02:17,570 --> 00:02:19,967 And working inter center to develop 67 00:02:20,002 --> 00:02:21,712 that, to make that a reality is a 68 00:02:21,747 --> 00:02:24,232 key milestone to how we’re going 69 00:02:24,267 --> 00:02:26,200 to be doing rockets in the future. 70 00:02:26,235 --> 00:02:27,688 And I think a lot of people are 71 00:02:27,723 --> 00:02:28,816 going to be looking back on this 72 00:02:28,851 --> 00:02:31,616 partnership for future development