1 00:00:00,000 --> 00:00:04,885 MUSIC 2 00:00:04,920 --> 00:00:06,078 So we are getting ready to 3 00:00:06,113 --> 00:00:07,710 static fire the QM-1 static 4 00:00:07,745 --> 00:00:09,070 test motor. It's a full rocket 5 00:00:09,105 --> 00:00:10,318 booster, it's made of five 6 00:00:10,353 --> 00:00:11,598 segments pieced together…and 7 00:00:11,633 --> 00:00:13,045 that's important because we've 8 00:00:13,080 --> 00:00:14,430 added another length of a 9 00:00:14,465 --> 00:00:15,560 segment into this booster to 10 00:00:15,595 --> 00:00:16,798 make it bigger and better. A lot 11 00:00:16,833 --> 00:00:18,133 of planning and work is done 12 00:00:18,168 --> 00:00:19,206 ahead of time as we design 13 00:00:19,241 --> 00:00:20,630 these rocket boosters to get 14 00:00:20,665 --> 00:00:22,109 the propellant geometry just 15 00:00:22,144 --> 00:00:23,957 right. We know at any given 16 00:00:23,992 --> 00:00:25,149 time during the burn of that 17 00:00:25,184 --> 00:00:27,613 motor what the thrust is and 18 00:00:27,648 --> 00:00:29,445 what the profile of the 19 00:00:29,480 --> 00:00:30,797 pressure is inside that motor. 20 00:00:30,832 --> 00:00:32,596 So with the new thrust profile 21 00:00:32,631 --> 00:00:34,901 for the SLS boosters we've 22 00:00:34,936 --> 00:00:37,060 added an extra fin and changed 23 00:00:37,095 --> 00:00:38,573 some of the geometry of our 24 00:00:38,608 --> 00:00:39,772 propellant surfaces so we can 25 00:00:39,807 --> 00:00:41,253 burn more propellant at the 26 00:00:41,288 --> 00:00:42,947 beginning of the test, or at 27 00:00:42,982 --> 00:00:44,388 the beginning of the rocket 28 00:00:44,423 --> 00:00:46,316 firing. To get a solid rocket 29 00:00:46,351 --> 00:00:47,868 booster to burn we have an 30 00:00:47,903 --> 00:00:50,140 igniter at the front end that is 31 00:00:50,175 --> 00:00:51,524 like a small rocket itself, and 32 00:00:51,559 --> 00:00:52,875 it shoots a flame hundred and 33 00:00:52,910 --> 00:00:54,413 fifty feet down this entire 34 00:00:54,448 --> 00:00:55,940 rocket booster and it ignites 35 00:00:55,975 --> 00:00:57,152 all the surface of the 36 00:00:57,187 --> 00:00:58,564 propellant all at once. Once 37 00:00:58,599 --> 00:01:00,084 you ignite a solid rocket 38 00:01:00,119 --> 00:01:01,484 booster you can't stop it. You 39 00:01:01,519 --> 00:01:02,579 don't flip a switch to turn it 40 00:01:02,614 --> 00:01:03,675 on and off. At the same time 41 00:01:03,710 --> 00:01:04,923 you turn a knob to increase 42 00:01:04,958 --> 00:01:06,164 your thrust or decrease your 43 00:01:06,199 --> 00:01:07,227 thrust. That's why it's 44 00:01:07,262 --> 00:01:08,387 important to design this 45 00:01:08,422 --> 00:01:09,979 beforehand. So we can get the 46 00:01:10,014 --> 00:01:11,331 amount of thrust we need at each 47 00:01:11,366 --> 00:01:12,682 point during this two minute 48 00:01:12,717 --> 00:01:14,115 burn to reach the maximum thrust 49 00:01:14,150 --> 00:01:16,563 at given time points that we 50 00:01:16,598 --> 00:01:17,955 need. At the beginning of the 51 00:01:17,990 --> 00:01:19,923 burn is when we have the most 52 00:01:19,958 --> 00:01:21,339 thrust, about three and a half 53 00:01:21,374 --> 00:01:22,466 million pounds of thrust that 54 00:01:22,501 --> 00:01:23,522 we maintain for about twenty 55 00:01:23,557 --> 00:01:24,634 five seconds. It takes just 56 00:01:24,669 --> 00:01:26,378 over two minutes of rocket 57 00:01:26,413 --> 00:01:27,459 firing for the propellant to 58 00:01:27,494 --> 00:01:28,938 completely burn out. The 59 00:01:28,973 --> 00:01:30,338 propellant is burning really 60 00:01:30,373 --> 00:01:31,747 fast; it's got a certain rate 61 00:01:31,782 --> 00:01:33,361 that it's burning from inside 62 00:01:33,396 --> 00:01:35,482 out. So as every second goes by 63 00:01:35,517 --> 00:01:37,394 it's like one layer of that 64 00:01:37,429 --> 00:01:39,050 propellant is essentially being 65 00:01:39,085 --> 00:01:40,386 peeled away and shot out the 66 00:01:40,421 --> 00:01:41,618 end of that rocket motor. 67 00:01:41,653 --> 00:01:42,913 Rocket science is not easy. 68 00:01:42,948 --> 00:01:44,729 This is a complex booster; 69 00:01:44,764 --> 00:01:46,034 we spend a lot of time and 70 00:01:46,069 --> 00:01:47,665 effort to get this right. And 71 00:01:47,700 --> 00:01:49,449 this is the first qualification 72 00:01:49,484 --> 00:01:51,946 test of this kind of rocket…I'm 73 00:01:51,981 --> 00:01:53,785 very confident that this booster 74 00:01:53,820 --> 00:01:55,441 static test motor is going to