1 00:00:45,110 --> 00:00:43,750 how many missions can an orbiter window 2 00:00:47,190 --> 00:00:45,120 withstand 3 00:00:49,510 --> 00:00:47,200 that's a determination that must be made 4 00:00:51,110 --> 00:00:49,520 at the end of each flight 5 00:00:53,270 --> 00:00:51,120 in order to determine the flight 6 00:00:55,430 --> 00:00:53,280 worthiness of the six thermal orbiter 7 00:00:58,069 --> 00:00:55,440 windows each one must first be 8 00:01:00,229 --> 00:00:58,079 laboriously hand cleaned 9 00:01:04,630 --> 00:01:00,239 a haze makes on to the surfaces in the 10 00:01:08,630 --> 00:01:06,950 the cleaning process takes approximately 11 00:01:11,030 --> 00:01:08,640 a week of labor 12 00:01:15,990 --> 00:01:11,040 and only after the haze is removed can 13 00:01:21,109 --> 00:01:18,789 small scale debris impacts on orbit and 14 00:01:24,310 --> 00:01:21,119 booster separation exhaust result in 15 00:01:26,390 --> 00:01:24,320 damage to the windows 16 00:01:28,310 --> 00:01:26,400 a mylar is made for flight to flight 17 00:01:30,789 --> 00:01:28,320 comparisons 18 00:01:33,190 --> 00:01:30,799 the new defects are evaluated using an 19 00:01:35,270 --> 00:01:33,200 epoxy mold impression 20 00:01:37,510 --> 00:01:35,280 any crater depth exceeding six ten 21 00:01:38,830 --> 00:01:37,520 thousandths of an inch results in a 22 00:01:41,510 --> 00:01:38,840 window 23 00:01:43,590 --> 00:01:41,520 replacement a new inspection system has 24 00:01:46,870 --> 00:01:43,600 been developed by the inet special 25 00:01:49,270 --> 00:01:46,880 instrumentation laboratory at ksc 26 00:01:51,830 --> 00:01:49,280 a lightweight scanning frame automates 27 00:01:53,830 --> 00:01:51,840 the side light optical scattering method 28 00:01:56,310 --> 00:01:53,840 and shows defects in the presence of 29 00:02:01,429 --> 00:01:58,709 this automated optical technique can be 30 00:02:03,350 --> 00:02:01,439 performed prior to polishing the windows 31 00:02:07,109 --> 00:02:03,360 and it provides a permanent and accurate 32 00:02:12,309 --> 00:02:09,350 a computer image can be printed onto a 33 00:02:16,630 --> 00:02:12,319 mylar and archived in a database for 34 00:02:20,949 --> 00:02:18,470 the second phase of the automated 35 00:02:23,430 --> 00:02:20,959 inspection employs a high resolution 36 00:02:28,550 --> 00:02:23,440 camera system to determine a maximum 37 00:02:33,670 --> 00:02:31,190 by adapting technologies already in use 38 00:02:34,869 --> 00:02:33,680 in shuttle and payloads defect analysis 39 00:02:36,949 --> 00:02:34,879 at ksc