1 00:00:13,290 --> 00:00:18,250 The uprated Saturn I Quarterly Film Report Number 28 covers progress during het period 2 00:00:18,250 --> 00:00:28,849 April, May, June 1966. 3 00:00:28,849 --> 00:00:33,840 In preparation for the launch of AS-203, the Chrysler-built booster for the second uprated 4 00:00:33,840 --> 00:00:39,410 Saturn I launch vehicle was whipped from Marshall’s Michoud Facility on April 7. 5 00:00:39,410 --> 00:00:42,290 It Arrived at Cape Kennedy five days later. 6 00:00:42,290 --> 00:00:46,750 It was moved into hanger AF for pre-erection inspection and checkout. 7 00:00:46,750 --> 00:00:52,470 On April 18, the stage was erected on LC 37B. 8 00:00:52,470 --> 00:00:57,740 On April 4, the Douglas-built second stage was flown from the west coast to Cape Kennedy, 9 00:00:57,740 --> 00:01:03,690 marking the first delivery of flight-type second stage aboard the Super Guppy. 10 00:01:03,690 --> 00:01:08,060 On April 14, the instrument unit was flown from Marshall to the Cape aboard the Super 11 00:01:08,060 --> 00:01:10,220 Guppy. 12 00:01:10,220 --> 00:01:17,130 The nosecone was barged from Marshall to KSC aboard the Poseidon last quarter. 13 00:01:17,130 --> 00:01:22,140 On April 21, the second stage, instrument unit, and nosecone were attacked atop the 14 00:01:22,140 --> 00:01:23,140 booster. 15 00:01:23,140 --> 00:01:29,360 Prelaunch activities for AS-203 then got underway and continued through the quarter. 16 00:01:29,360 --> 00:01:34,400 The prime mission of AS-203 will be to place the second stage with about ten tons of liquid 17 00:01:34,400 --> 00:01:38,670 hydrogen into ta circular orbit of 100 nautical miles. 18 00:01:38,670 --> 00:01:43,310 This will allow Marshall space scientists to study the dynamics of liquid hydrogen under 19 00:01:43,310 --> 00:01:48,600 weightlessness and verify that the stage’s engine can be restarted in orbit. 20 00:01:48,600 --> 00:01:54,850 Objectives of the tests include determining if the continuous venting system and thrusters 21 00:01:54,850 --> 00:01:59,150 will properly seep the liquid hydrogen in the bottom of the tanks and if the engine 22 00:01:59,150 --> 00:02:06,490 can be adequately chilled down to simulate Saturn V S-IVB orbital operations. 23 00:02:06,490 --> 00:02:11,040 At Marshall’s System Development Facility, in unison with Launch Preparations at Kennedy 24 00:02:11,040 --> 00:02:17,069 Space Center, work efforts continued on development and verification of the computer program tapes 25 00:02:17,069 --> 00:02:18,400 of automatic checkout of AS-203. 26 00:02:18,400 --> 00:02:24,909 AS-203 is scheduled for launch on July 5. 27 00:02:24,909 --> 00:02:31,239 Following completion of vehicle erection at Launch Complex 34 last quarter, SA-202 continued 28 00:02:31,239 --> 00:02:34,549 in preflight checkout throughout the report period. 29 00:02:34,549 --> 00:02:37,719 AS-202 launch is planned for next quarter. 30 00:02:37,719 --> 00:02:42,950 Its mission will be to launch the Apollo spacecraft into suborbital flight ending in the Pacific 31 00:02:42,950 --> 00:02:45,120 Ocean near Wake Island. 32 00:02:45,120 --> 00:02:49,659 During reentry, the spacecraft ablative heat shield will be tested under the high heat 33 00:02:49,659 --> 00:02:57,239 loads of reentry. 34 00:02:57,239 --> 00:03:01,239 At Marshall’s Michoud Assembly Facility, Chrysler completed post-static checkout May 35 00:03:01,239 --> 00:03:04,430 25 on the booster for the fourth flight vehicle. 36 00:03:04,430 --> 00:03:09,010 The stage is scheduled for shipment to the Cape next quarter. 37 00:03:09,010 --> 00:03:13,290 Following he second successful static firing, a leak was detected inside the thrust chamber 38 00:03:13,290 --> 00:03:17,379 on engine position number four of the fifth flight booster. 39 00:03:17,379 --> 00:03:21,439 Investigation revealed a horizontal crack in a tube about ten inches below the injector 40 00:03:21,439 --> 00:03:22,439 face. 41 00:03:22,439 --> 00:03:26,700 The engine was removed and shipped to Rocketdyne Neosho for a repair. 42 00:03:26,700 --> 00:03:31,400 The booster was shipped back to Michoud on April 7, arriving six days later. 43 00:03:31,400 --> 00:03:36,790 Modification was performed, including replacement of the repaired engine, and post-static checkout 44 00:03:36,790 --> 00:03:40,680 began on May 31. 45 00:03:40,680 --> 00:03:44,969 Pre-static checkout of the six flight vehicle booster was completed early this quarter. 46 00:03:44,969 --> 00:03:49,769 The stage was shipped to Marshall from Michoud May 19, arriving May 28. 47 00:03:49,769 --> 00:03:53,169 It was installed in the Static Test Stand May 31. 48 00:03:53,169 --> 00:03:58,819 A short-duration firing was conducted June 23, followed by a long-duration firing June 49 00:03:58,819 --> 00:03:59,819 29. 50 00:03:59,819 --> 00:04:05,040 This test series marks another milestone in the Saturn IB Program since the Rocketdyne-built 51 00:04:05,040 --> 00:04:09,450 engines have been uprated to 205,000 pounds thrust. 52 00:04:09,450 --> 00:04:14,559 No problems were encountered except for a thrust chamber leak on one engine, which necessitated 53 00:04:14,559 --> 00:04:16,800 engine removal for a repair. 54 00:04:16,800 --> 00:04:22,130 A replacement engine was installed to preserve schedule, and the stage is undergoing preparation 55 00:04:22,130 --> 00:04:26,919 for shipment to Michoud, planned for next quarter. 56 00:04:26,919 --> 00:04:31,600 Assembly of the first stage for the seventh flight vehicle was completed in mid-quarter. 57 00:04:31,600 --> 00:04:36,820 Pre-static checkout got underway May 31, about two and one-half weeks ahead of schedule. 58 00:04:36,820 --> 00:04:41,510 Checkout is scheduled for completion early next quarter. 59 00:04:41,510 --> 00:04:45,020 Fabrication of the eighth flight booster was completed early this quarter. 60 00:04:45,020 --> 00:04:52,120 Stage assembly started April 14 and is scheduled for completion early next quarter. 61 00:04:52,120 --> 00:04:55,220 Fabrication of the ninth flight vehicle was completed in June. 62 00:04:55,220 --> 00:04:57,090 Assembly is underway. 63 00:04:57,090 --> 00:05:01,750 Also at Michoud, fabrication of the tenth flight vehicle was started in early April 64 00:05:01,750 --> 00:05:05,810 and continued throughout the report period. 65 00:05:05,810 --> 00:05:10,700 Chrysler has only two more boosters remaining to be manufactured under the present contract. 66 00:05:10,700 --> 00:05:14,650 All of the long lead time items for these two have been procured. 67 00:05:14,650 --> 00:05:20,610 First stage LOX tank qualification testing continued early this quarter by Chrysler at 68 00:05:20,610 --> 00:05:21,690 Michoud. 69 00:05:21,690 --> 00:05:28,120 Both the seventy inch and the 105 inch tanks were tested to 125 percent design load, meeting 70 00:05:28,120 --> 00:05:32,520 test completion deadline and requirements for SA-203. 71 00:05:32,520 --> 00:05:38,360 Additional testing is being conducted to qualify the tanks to 140 percent design load for manned 72 00:05:38,360 --> 00:05:39,430 flight reliability. 73 00:05:39,430 --> 00:05:46,020 The 105 inch LOX tank has been tested to 140 percent of design load under all condition 74 00:05:46,020 --> 00:05:47,370 except two. 75 00:05:47,370 --> 00:05:56,460 The seventy inch tank has been qualified under all conditions except maximum thin load. 76 00:05:56,460 --> 00:06:04,730 Meanwhile, at Douglas’ SACTO Facility, the second stage for the fourth flight vehicle 77 00:06:04,730 --> 00:06:10,470 underwent modification, rework, and post-static checkout at the vertical checkout laboratory. 78 00:06:10,470 --> 00:06:14,770 The stage was accepted by Marshall at SACTO on May 6. 79 00:06:14,770 --> 00:06:18,340 Shipment to Cape Kennedy will be next quarter. 80 00:06:18,340 --> 00:06:22,710 The second stage for the fifth flight vehicle was shipped from Huntington Beach to SACTO 81 00:06:22,710 --> 00:06:24,030 April 9. 82 00:06:24,030 --> 00:06:29,810 On April 13, the stage was installed in the Beta 3 Test Stand where pre-static and subsystem 83 00:06:29,810 --> 00:06:32,560 checkout proceeded at scheduled. 84 00:06:32,560 --> 00:06:38,810 Following a successful 440second acceptance firing on June 2, post-static checkout was 85 00:06:38,810 --> 00:06:43,030 completed June 28. 86 00:06:43,030 --> 00:06:47,470 Following installation of the J-2 engine in April for the sixth flight vehicle second 87 00:06:47,470 --> 00:06:52,810 stage and factory checkout completion in late May, final inspection was made and the stage 88 00:06:52,810 --> 00:06:55,340 was shipped to SACTO June 30. 89 00:06:55,340 --> 00:07:01,050 In April, Douglas completed joining of the thrust structure and forward and aft skirts 90 00:07:01,050 --> 00:07:06,600 of the second stage of the seventh flight vehicle and installed the engine in May. 91 00:07:06,600 --> 00:07:10,620 Factory checkout was started and continued through the report period. 92 00:07:10,620 --> 00:07:14,720 Completion of checkout is scheduled for early next quarter. 93 00:07:14,720 --> 00:07:19,080 The second stage of the eighth flight vehicle was removed from the insulation chamber on 94 00:07:19,080 --> 00:07:20,330 June 6. 95 00:07:20,330 --> 00:07:25,590 Necessary cleaning and miscellaneous parts installations were completed in June. 96 00:07:25,590 --> 00:07:30,280 Factory checkout will take place next quarter. 97 00:07:30,280 --> 00:07:33,650 Manufacturing was completed on the common bulkhead for the second stage of the ninth 98 00:07:33,650 --> 00:07:35,900 flight vehicle at Santa Monica. 99 00:07:35,900 --> 00:07:40,950 Welding of the liquid hydrogen tank segments and LOX tank assemblies was completed and 100 00:07:40,950 --> 00:07:44,840 the LOX tank was shipped to Huntington Beach June 16. 101 00:07:44,840 --> 00:07:49,680 Stage assembly will be completed next quarter. 102 00:07:49,680 --> 00:07:53,740 Fabrication of the tenth flight vehicle’s second stage was started last quarter and 103 00:07:53,740 --> 00:07:58,139 was drawing to a successful close at the end of this report period. 104 00:07:58,139 --> 00:08:03,180 Assembly and miscellaneous testing is planned for next quarter. 105 00:08:03,180 --> 00:08:09,139 On April 13 at SACTO during S-IVB structural testing, the common bulkhead and LOX tank 106 00:08:09,139 --> 00:08:10,340 failed. 107 00:08:10,340 --> 00:08:14,740 The failure is being thoroughly investigated by Marshall and Douglas personnel. 108 00:08:14,740 --> 00:08:20,360 However, subsequent structural testing on the hydrostatic test tank specimen qualified 109 00:08:20,360 --> 00:08:28,960 the design. 110 00:08:28,960 --> 00:08:33,729 At IBM Huntsville, component installation in the fourth flight instrument unit, started 111 00:08:33,729 --> 00:08:37,450 last period, was completed the first week in May. 112 00:08:37,450 --> 00:08:39,940 Checkout began in May and was completed on June 28. 113 00:08:39,940 --> 00:08:46,240 The unit will be shipped from IBM to the Cape early next quarter. 114 00:08:46,240 --> 00:08:52,449 The fifth flight IU structural fabrication started last quarter was completed May 4. 115 00:08:52,449 --> 00:08:59,290 Component installation was begun ten days later with completion planned for next quarter. 116 00:08:59,290 --> 00:09:04,009 Also at IBM Huntsville, structural fabrication was started for the sixth flight instrument 117 00:09:04,009 --> 00:09:11,170 unit. 118 00:09:11,170 --> 00:09:18,180 At Marshall, work effort is underway for in-house manufacture of four uprated Saturn I nosecones. 119 00:09:18,180 --> 00:09:24,850 These units will be carried atop the vehicles which will place lunar modules into orbit. 120 00:09:24,850 --> 00:09:28,959 In late April, ten astronauts visited the Marshall Center for briefings on the uprated 121 00:09:28,959 --> 00:09:30,709 Saturn I Program. 122 00:09:30,709 --> 00:09:36,370 Among the group are the three men who will fly the first manned Saturn, Apollo 1B Mission, 123 00:09:36,370 --> 00:09:42,639 Virgil Grissom, Command Pilot, Edward White, and Roger Chaffee. 124 00:09:42,639 --> 00:09:47,870 The astronauts were given briefings, including primary hardware description and design philosophy 125 00:09:47,870 --> 00:09:51,110 by Saturn engineers and management officials. 126 00:09:51,110 --> 00:09:55,470 The astronauts also studied flight data on the performance of the first uprated Saturn 127 00:09:55,470 --> 00:10:01,970 I, which launched an unmanned Apollo spacecraft last quarter. 128 00:10:01,970 --> 00:10:07,350 A summary of the Saturn IB program through the months April, May, and June shows major 129 00:10:07,350 --> 00:10:15,559 accomplishments in all areas, continued buildup of Saturn IB stages and equipment, acceleration