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Saturn one 1d quarterly film report

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number 21 covers progress during the

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period July August September 1964 the

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leading of that of the report period was

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the successful launch in flight of the

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seventh Saturn sa seven sa seven booster

7
00:00:36,799 --> 00:00:34,410
check out at Cape Kennedy were slowed

8
00:00:38,840 --> 00:00:36,809
down in early July when the eight h1

9
00:00:42,319 --> 00:00:38,850
engines were removed for LOX dome

10
00:00:44,540 --> 00:00:42,329
replacement MSFC decided to replace the

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dome after investigating the stress

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corrosion cracking in the dome of engine

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number seven rocket dines Neosho

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Missouri plant performed the dome

15
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replacement the remainder of the

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checkout was routine except for two

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brief delays by hurricanes sa seven

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countdown started in the early morning

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of September 18th liftoff occurred at

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11:22 a.m. Eastern Standard Time the

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00:01:11,929 --> 00:01:09,450
payload a boilerplate Apollo spacecraft

22
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and flight missions were very similar to

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those of si6 successfully launched last

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quarter the launch vehicle contained

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minor changes made to improve overall

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performance sa seven flight objectives

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included retesting a vehicle propulsion

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structural guidance in flight control

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systems and providing additional data on

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Apollo boilerplate behavior during

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powered flight in addition the

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spacecraft launch escape system was

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successfully jettisoned and the s4's

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recently added non propulsive vent

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systems successfully tested the purpose

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of this new vent system is to reduce

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payload spin and tumble this was the

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seventh straight successful flight of

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the Marshall engineered Saturn s1 stage

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and the third straight successful s4

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flight the three remaining R&D flight

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test vehicles will carry the large

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meteoroid technology satellite recently

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named Pegasus

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for the first time the st 124 guidance

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system platform was in complete control

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of the entire vehicle s for stage flight

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was as expected the boilerplate

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00:02:24,870 --> 00:02:22,360
spacecraft was successfully placed into

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a low orbit closely approximating the

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parking orbit for future manned

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exploration missions at fairchild hiller

53
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the pegasus prototype spacecraft is

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structurally and mechanically complete

55
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however installation of electronic

56
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systems has been delayed because of

57
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development problems as a result Pegasus

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a will be launched by sa9 as an

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operational engineering test model

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Pegasus B to be launched later by si8

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will be the first fully flight qualified

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meteoroid satellite Marshall is

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presently re-evaluating the entire

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Pegasus program scheduled as a result of

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the h1 engine LOX dome problem sa 9

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booster final check out at Marshall was

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discontinued for about one month until

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the engine domes had been replaced

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staged checkout was then resumed and

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completed late in the quarter shipment

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00:03:23,760 --> 00:03:21,239
to Cape Kennedy is scheduled for October

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following successful static firings at

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Marshall the Chrysler built s18 was

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shipped back to miss you arriving on

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June 28 repair operations and

76
00:03:36,570 --> 00:03:33,040
modifications were completed late this

77
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quarter LOX dome retrofit of all engines

78
00:03:41,220 --> 00:03:39,580
was also completed stage post static

79
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checkout is scheduled to begin in

80
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October the booster for the tenth flight

81
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vehicle s 110 was shipped from Chrysler

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Michou and directed in Marshall static

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test and LOX dome retrofit of the

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engines was accomplished and preparation

85
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for static firing began in early

86
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September on September 24th the stage

87
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successfully completed the first of two

88
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flight acceptance firings following the

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second acceptance firing the booster

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will be shipped back to Mishu for

91
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routine modification and repair

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operations and post static checkout s110

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is

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at Doug mrs. sacto test facility s 49

95
00:04:32,110 --> 00:04:29,810
underwent a new weighing procedure in

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this new program the stage is covered

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with a plastic bag warm air is

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circulated around the stage preventing

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00:04:42,189 --> 00:04:39,530
frost build-up allowing more accurate

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cryogenic propellant weighing with this

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data a more precise orbital trajectory

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can be calculated on August 6th a

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00:04:57,040 --> 00:04:54,650
successful acceptance firing was

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performed the stage was then removed

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from the stand and installation and

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check out of the non propulsive venting

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system were begun s 4/9 is presently

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undergoing preparations for shipment to

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Cape Kennedy on August 28 the S 4 8

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00:05:16,629 --> 00:05:14,090
stage was erected on test stand to be

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and acceptance firing test preparations

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including cryogenic propellant weighing

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were begun at santa monica s410 stage

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checkout is nearing completion

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preparations for acceptance firing is

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scheduled to begin next quarter at

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Marshall SIU 9 pre-flight check out was

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completed in mid-september the unit is

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being prepared for shipment to KSC with

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s-19 siu 8th component installation

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continued during the quarter with

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checkout scheduled to start early next

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quarter siu 10 structure was removed

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from storage and component installation

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started in mid-september at Marshall the

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last phase of the dynamic test program

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was finished in July with a successful

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completion of the sa nine eight and ten

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vehicle configuration tests following

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completion of the Saturn one dynamic

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test program the sa D 5 first stage was

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shipped to Chrysler Michou for

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modification to s 1 B D F design the

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booster has been weighed to determine

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the longitudinal center of gravity

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necessary ballast will be placed in the

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stage to relocate the center of gravity

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to the s-1 b1

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figuration following the weighing

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Chrysler began removing components in

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tanks to tanks the 105 inch LOX tank and

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one fuel tank were shipped to Ling temp

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Co bought Dallas Texas for a

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modification the components earmarked

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for the s-1 BDF have been labeled

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wrapped hermetically sealed and stored

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in late September build-up of the s-1

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btf stage started with the modified

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flight tail section new spider beam the

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modified tanks and the usable si d5

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components also Michou chrysler assembly

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operations on the s-1 b1 continued

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unschedule all eight operated h1 engines

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have been installed pre static check out

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of the stage is expected to begin in

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November s 1 b2 fabrication operations

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were completed and clustering began in

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late September s1 b3 fabrication began

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in July tail section assembly operations

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are proceeding with clustering scheduled

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for late next quarter at Huntington

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Beach California

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Douglas completed installation of

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additional instrumentation in the s4 be

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structural test stage Marshall had

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requested this instrumentation to

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provide more complete data in event of a

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rupture on July 14th the stages liquid

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hydrogen tank did ruptured during

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hydrostatic testing the failure caused

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by an incomplete weld fusion occurred at

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34 psi g2 psig less than proof pressure

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for this test with this additional

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instrumentation enough test data was

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recorded to eliminate the necessity for

176
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additional LH to tank structural testing

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the necessary testing of the thrust

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structure will be performed with the

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repaired LOX tank and common bulkhead

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insulation of the s4 be dynamic stage

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was completed in July installation of

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simulated systems and staged checkout is

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underway assembly of the old system

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stage has been completed and the stage

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moved into insulation chamber number one

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this activity is scheduled to be

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completed in October as a result of the

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Apollo program assessment the all

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systems test program will

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terminated upon completion of propellant

191
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loading tests the stage has been

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redesignated as a facilities checkout

193
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stage assembly of the original

194
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facilities checkout stage was completed

195
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this quarter following installation of

196
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the stage scheduled for next quarter

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further work will be stopped and the

198
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stage stored until the decision can be

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made about assigning other program

200
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missions to the stage at Douglass's

201
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Santa Monica and Huntington Beach

202
00:09:21,240 --> 00:09:16,210
facilities fabrication and assembly of

203
00:09:22,950 --> 00:09:21,250
the s4 b-1b stages continued at

204
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Huntington Beach insulation is being

205
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applied to the tanks of the first flight

206
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stage 201 with completion scheduled for

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early next quarter tank assembly and

208
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proof testing for the second flight

209
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stage 202 are complete insulation

210
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operations will be in process next

211
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quarter fabrication and assembly of the

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propellant tanks and thrust structures

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for the third and fourth flight stages

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203 and 204 are underway at the

215
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Sacramento test area dub discontinued

216
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preparing for the first s4b battleship

217
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hot firing at the end of last quarter

218
00:10:03,690 --> 00:10:01,330
douglas completed installing a j2 engine

219
00:10:06,210 --> 00:10:03,700
on the battleship test stage following

220
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this the stage was prepared for cold

221
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flow testing the first hot firing is

222
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scheduled for next quarter other efforts

223
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leading to the hot firing included

224
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completing checkout of the battleship

225
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ground support equipment at the sacto

226
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site the sacto gamma test facility to be

227
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used for testing s4b attitude control

228
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engines has been completed several

229
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engines were received from the Tapco

230
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plant at Cleveland Ohio and are being

231
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installed on the test stems the first

232
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firing test is scheduled for next

233
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quarter Saturn 1b instrument unit

234
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structure redesign necessitated by

235
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revised vehicle loads was completed in

236
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August structural units already

237
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delivered for the old design will be

238
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used for Saturn 1b and five tests not

239
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affected by the change the first

240
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redesigned IU structure will be

241
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delivered to Marshall next quarter

242
00:11:04,620 --> 00:11:01,660
by General Dynamics Fort Worth Texas

243
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this unit will be used in the Saturn 1b

244
00:11:12,329 --> 00:11:09,700
and five dynamic test programs at MSFC

245
00:11:14,430 --> 00:11:12,339
an IU environmental control system

246
00:11:16,980 --> 00:11:14,440
prototype heat exchanger was

247
00:11:19,230 --> 00:11:16,990
successfully tested the heat exchanger

248
00:11:22,019 --> 00:11:19,240
would provide temperature control during

249
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flight for the IU equipment and for

250
00:11:27,720 --> 00:11:24,940
equipment in the s4b stage forward skirt

251
00:11:29,970 --> 00:11:27,730
area the cooling method utilizes a

252
00:11:31,890 --> 00:11:29,980
solution of water methanol which

253
00:11:36,000 --> 00:11:31,900
circulates through the cold plates on

254
00:11:38,160 --> 00:11:36,010
which the components are mounted also at

255
00:11:40,740 --> 00:11:38,170
Marshall mounting of components on the

256
00:11:43,290 --> 00:11:40,750
IU structure for Saturn 1b and five

257
00:11:45,450 --> 00:11:43,300
vibration tests began in early September

258
00:11:47,880 --> 00:11:45,460
and is expected to be completed in

259
00:11:49,980 --> 00:11:47,890
October fabrication of redesigned

260
00:11:53,010 --> 00:11:49,990
structural segments for the Saturn 1b

261
00:11:55,230 --> 00:11:53,020
and five dynamic test unit began July

262
00:11:57,600 --> 00:11:55,240
1st at Fort Worth and continued

263
00:11:59,550 --> 00:11:57,610
throughout the quarter contract

264
00:12:01,890 --> 00:11:59,560
negotiations are still in progress with

265
00:12:04,610 --> 00:12:01,900
International Business Machines recently

266
00:12:07,560 --> 00:12:04,620
selected as prime contractor for the IU

267
00:12:09,329 --> 00:12:07,570
IBM has been authorized to proceed with

268
00:12:12,690 --> 00:12:09,339
its efforts in personnel and facilities

269
00:12:14,730 --> 00:12:12,700
buildup at Huntsville at Marshall

270
00:12:16,380 --> 00:12:14,740
testing continued on various ground

271
00:12:19,500 --> 00:12:16,390
support equipment for the Kennedy Space

272
00:12:24,329 --> 00:12:19,510
Center such as this prototype s4b aft

273
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swing arm assembly also at Marshall the

274
00:12:29,100 --> 00:12:26,320
Saturn system development facility is

275
00:12:31,019 --> 00:12:29,110
being enlarged to accommodate Saturn 1b

276
00:12:33,780 --> 00:12:31,029
ground support equipment and stage

277
00:12:36,269 --> 00:12:33,790
simulators the facility is used for

278
00:12:38,030 --> 00:12:36,279
checkout tape development GSE and

279
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vehicle system debugging and

280
00:12:42,960 --> 00:12:41,200
certification of systems integration the

281
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delivery and installation of some

282
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consoles is underway and will continue

283
00:12:49,500 --> 00:12:46,779
throughout the year

284
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the remaining GSE and flight simulation

285
00:12:54,150 --> 00:12:50,980
equipment will be delivered and

286
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installed early in 1965 greater

287
00:13:00,810 --> 00:12:56,380
versatility will be provided for Saturn

288
00:13:05,130 --> 00:13:00,820
1b operations by 2rc a 110 a computers

289
00:13:07,230 --> 00:13:05,140
connected in a tandem mode also at MSFC

290
00:13:09,900 --> 00:13:07,240
construction of the j2 engine test

291
00:13:11,730 --> 00:13:09,910
facility is about 90% complete with

292
00:13:13,800 --> 00:13:11,740
beneficial occupancy expected in

293
00:13:16,080 --> 00:13:13,810
November the facility will be

294
00:13:20,300 --> 00:13:16,090
used for various test programs using a

295
00:13:22,860 --> 00:13:20,310
Marshall built battleship s4p unit

296
00:13:25,680 --> 00:13:22,870
meanwhile at Rocketdyne at Canoga Park

297
00:13:27,990 --> 00:13:25,690
California assembly a flexible armor

298
00:13:30,150 --> 00:13:28,000
clad harnesses for all j2 engine

299
00:13:32,820 --> 00:13:30,160
electrical control and instrumentation

300
00:13:35,579 --> 00:13:32,830
harness wiring is underway this will

301
00:13:37,800 --> 00:13:35,589
provide the 14 individual j2 engine

302
00:13:39,750 --> 00:13:37,810
harness assemblies with handling and

303
00:13:45,210 --> 00:13:39,760
abrasion protection moisture protection

304
00:13:47,280 --> 00:13:45,220
and short-term fire protection in a

305
00:13:50,160 --> 00:13:47,290
series of successful tests the gun last

306
00:13:52,110 --> 00:13:50,170
report period the Rocketdyne j2 engine

307
00:13:53,790 --> 00:13:52,120
has demonstrated its ability to meet

308
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preliminary flight rating test

309
00:14:01,470 --> 00:13:56,140
requirements for gimble incurring hot

310
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firing in summary July August and

311
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September four months of significant

312
00:14:09,630 --> 00:14:07,290
progress in the Saturn one 1b program

313
00:14:12,570 --> 00:14:09,640
highlighting this quarter was the

314
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successful flight of Saturn 7 and the

315
00:14:18,329 --> 00:14:14,950
successful completion of the Saturn one

316
00:14:20,790 --> 00:14:18,339
dynamic test program in the Saturn 1b

317
00:14:24,690 --> 00:14:20,800
program emphasis was placed on

318
00:14:27,690 --> 00:14:24,700
contractor efforts s4v ground and flight

319
00:14:30,200 --> 00:14:27,700
stage assembly continued ground support

320
00:14:33,180 --> 00:14:30,210
equipment build-up engine programs