1 00:00:00,000 --> 00:00:11,047 Music.60's Surf Music 2 00:00:11,047 --> 00:00:12,003 NARRATOR: It's the mid 3 00:00:12,003 --> 00:00:13,093 1960's, and the Apollo 4 00:00:13,093 --> 00:00:15,023 Program is testing its 5 00:00:15,023 --> 00:00:16,067 Launch Escape System. 6 00:00:16,067 --> 00:00:18,033 At the White Sands Missile 7 00:00:18,033 --> 00:00:19,063 Range in Las Cruces New 8 00:00:19,063 --> 00:00:21,017 Mexico, a squatty rocket 9 00:00:21,017 --> 00:00:23,010 nicknamed Little Joe 2 10 00:00:23,010 --> 00:00:24,093 launches an Apollo capsule 11 00:00:24,093 --> 00:00:28,023 for a high altitude test. 12 00:00:28,023 --> 00:00:29,020 Engineers want to see if 13 00:00:29,020 --> 00:00:30,060 the escape system can pull 14 00:00:30,060 --> 00:00:31,077 the capsule away from 15 00:00:31,077 --> 00:00:33,007 danger in the event of an 16 00:00:33,007 --> 00:00:34,057 emergency. 17 00:00:34,057 --> 00:00:35,070 The unmanned test shows 18 00:00:35,070 --> 00:00:37,063 the escape system works! 19 00:00:41,020 --> 00:00:42,030 Years later, an escape 20 00:00:42,030 --> 00:00:43,060 system was used for real 21 00:00:43,060 --> 00:00:45,067 on a Russian Soyuz rocket. 22 00:00:45,067 --> 00:00:47,020 When spilt fuel caught 23 00:00:47,020 --> 00:00:49,007 fire on the launch pad, an 24 00:00:49,007 --> 00:00:50,037 escape rocket pulled the 25 00:00:50,037 --> 00:00:51,083 crew away from the hazard, 26 00:00:51,083 --> 00:00:54,053 saving their lives. 27 00:00:54,053 --> 00:00:56,077 For Orion, crew safety is 28 00:00:56,077 --> 00:00:58,010 a prime factor in its 29 00:00:58,010 --> 00:00:59,053 design. 30 00:00:59,053 --> 00:01:00,073 Engineers have included a 31 00:01:00,073 --> 00:01:02,033 Launch Abort System which 32 00:01:02,033 --> 00:01:03,047 is more robust and 33 00:01:03,047 --> 00:01:04,087 features more control 34 00:01:04,087 --> 00:01:06,057 capability than any of its 35 00:01:06,057 --> 00:01:09,040 predecessors 36 00:01:09,040 --> 00:01:10,063 Once again, 37 00:01:10,063 --> 00:01:11,090 the White Sands Missile 38 00:01:11,090 --> 00:01:13,023 Range will play host to 39 00:01:13,023 --> 00:01:14,040 the escape system flight 40 00:01:14,040 --> 00:01:15,063 tests. 41 00:01:15,063 --> 00:01:17,043 A mock crew module will 42 00:01:17,043 --> 00:01:18,060 sit in for the Orion 43 00:01:18,060 --> 00:01:20,023 spacecraft. 44 00:01:20,023 --> 00:01:21,037 Instead of a crew, a 45 00:01:21,037 --> 00:01:22,067 battery of sensors are 46 00:01:22,067 --> 00:01:24,030 installed inside to help 47 00:01:24,030 --> 00:01:26,053 analyze the flight. 48 00:01:26,053 --> 00:01:28,013 Called Pad Abort-1, the 49 00:01:28,013 --> 00:01:29,063 test will simulate an 50 00:01:29,063 --> 00:01:31,050 abort off the Ares I, 51 00:01:31,050 --> 00:01:32,047 while it is still sitting 52 00:01:32,047 --> 00:01:33,083 on the launch pad. 53 00:01:33,097 --> 00:01:34,067 Because an abort must 54 00:01:34,067 --> 00:01:36,050 happen quickly, the entire 55 00:01:36,050 --> 00:01:38,030 test will take place in a 56 00:01:38,030 --> 00:01:41,007 matter of seconds... 57 00:01:41,007 --> 00:01:41,063 Don Reed:"So the first 58 00:01:41,063 --> 00:01:42,057 thing that happens is we 59 00:01:42,057 --> 00:01:44,037 fire, send a command to 60 00:01:44,037 --> 00:01:46,007 fire the abort motor and, 61 00:01:46,007 --> 00:01:47,027 at the same time, we fire 62 00:01:47,027 --> 00:01:48,063 the command, send the 63 00:01:48,063 --> 00:01:49,037 command to fire the 64 00:01:49,037 --> 00:01:50,073 attitude control motor. 65 00:01:50,073 --> 00:01:52,060 So right off the bat we, 66 00:01:52,060 --> 00:01:53,067 we put out five hundred 67 00:01:53,067 --> 00:01:54,050 thousand pounds of thrust 68 00:01:54,050 --> 00:01:56,000 and in the first two 69 00:01:56,000 --> 00:01:57,050 seconds we accelerate to 70 00:01:57,050 --> 00:02:00,080 about Mach point six... 71 00:02:00,080 --> 00:02:02,010 about ten seconds we send 72 00:02:02,010 --> 00:02:04,000 the command to reorient... 73 00:02:04,000 --> 00:02:04,077 what'll happen then is 74 00:02:04,077 --> 00:02:05,060 that the attitude control 75 00:02:05,060 --> 00:02:07,000 motor will then start to 76 00:02:07,000 --> 00:02:08,043 pitch the vehicle over and 77 00:02:08,043 --> 00:02:10,010 reorient it ...we're now 78 00:02:10,010 --> 00:02:11,030 flying that the heat 79 00:02:11,030 --> 00:02:12,023 shield is now forward into 80 00:02:12,023 --> 00:02:14,053 the air stream. 81 00:02:14,053 --> 00:02:16,057 At twenty-one seconds 82 00:02:16,057 --> 00:02:17,070 we'll go ahead and fire 83 00:02:17,070 --> 00:02:19,013 the jettison motor which 84 00:02:19,013 --> 00:02:20,030 then jettisons this whole 85 00:02:20,030 --> 00:02:21,053 tower so now you just have 86 00:02:21,053 --> 00:02:22,077 the, the crew module 87 00:02:22,077 --> 00:02:25,003 flying by itself. 88 00:02:25,003 --> 00:02:26,000 Twenty-three seconds, 89 00:02:26,000 --> 00:02:27,017 we'll then jettison the 90 00:02:27,017 --> 00:02:28,067 forward bay cover and then 91 00:02:28,067 --> 00:02:30,027 two seconds later, at 92 00:02:30,027 --> 00:02:31,040 twenty-five seconds, we'll 93 00:02:31,040 --> 00:02:32,063 deploy the drogue chutes. 94 00:02:32,063 --> 00:02:34,047 And then for the next 95 00:02:34,047 --> 00:02:35,063 fifty seconds we're 96 00:02:35,063 --> 00:02:36,067 basically descending in 97 00:02:36,067 --> 00:02:38,013 stable flight, under the 98 00:02:38,013 --> 00:02:40,000 three main parachutes. 99 00:02:40,000 --> 00:02:41,023 And so by testing this 100 00:02:41,023 --> 00:02:42,073 abort system, we directly 101 00:02:42,073 --> 00:02:45,003 influence the ability to 102 00:02:45,003 --> 00:02:48,037 keep the crew safe. 103 00:02:48,037 --> 00:02:49,027 It's what I've done my 104 00:02:49,027 --> 00:02:50,060 career is doing 105 00:02:50,060 --> 00:02:51,050 flight tests, so to 106 00:02:51,050 --> 00:02:52,050 actually be here and be 107 00:02:52,050 --> 00:02:53,083 part of this program and 108 00:02:53,083 --> 00:02:55,037 doing flight tests...I