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[Music]

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Saturn one 1b quarterly film report

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number 24 covers progress during the

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period April May June 1965 highlighting

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this quarter was the successful launch

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in flight of the night Saturn one si8

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and the equally successful orbiting of

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the second meteoroid technology

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satellite Pegasus B at the beginning of

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the quarter

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the launch vehicle had been erected at

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the Cape and was being tested on April

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10th following preparations for shipment

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the service module and its adapter for

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Apollo boilerplate number 26 was flown

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from Marshall to the Cape meanwhile

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final checkout of Pegasus B was

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completed at Hagerstown Maryland

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following checkout the satellite was

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shipped to General Electric for

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vibration tests April 13th two days

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later

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Pegasus B was shipped to the Cape in

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mid-april Pegasus B underwent system

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checks in hangar D following testing the

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satellite was mated to boiler plate

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number 26 is service module and it's

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adapter April 27th on April 28 the

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spacecraft was moved to the launch pad

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and directed atop si8 direction of the

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command module followed immediately

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flight objectives of si8 were to provide

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and evaluate meteoroid data in near

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Earth orbit demonstrate launch vehicle

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iterative guidance mode and evaluate

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system accuracy and test a closed-loop

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guidance system for the fourth time

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pre-launch check out of si8 progressed

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satisfactorily countdown demonstration

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test incompletes May 21st countdown

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vehicle liftoff occurred on May 25th at

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2:35 a.m. Eastern Standard Time si8 the

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first vehicle to use a chrysler built

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booster was the night straight

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successful Saturn the first stage burned

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the second stage burned about 474

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seconds obtaining programs cutoff

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velocity stage performance was

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satisfactory the Apollo command and

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service module jettisoned mechanically

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and the Pegasus wings successfully

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deployed Pegasus bees roll rate was six

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point six degrees per second as compared

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to Pegasus age roll rate of nine point

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eight degrees Pegasus B like its

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predecessor is successfully obtaining

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information concerning quantity and

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penetrating ability of meteoroids in the

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near-earth orbit the remaining Pegasus

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satellite will be launched by SI ten

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which throughout the quarter has been

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undergoing preparations for launch at

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Marshalls Michou operations preparations

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for shipment of s1 10 continued during

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April and May on May 26th the booster

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departed via barge for Cape Kennedy and

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two days later it was erected on the pad

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s410 was removed from storage at Sacto

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then loaded aboard the guppy and flown

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to KSC arriving may 8 inch a cow and

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necessary painting the stage was erected

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atop s110 the evening of June 8 check

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out of SIU 10 was completed in early

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April preparations for shipment of the

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instrument unit 4 completed April 16th

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when it was temporarily placed in

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storage on June 1st

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SIU 10 was delivered to the Cape on June

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night following checkout alignment and

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painting the unit was erected atop the

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stages pre-launch checkout of stages and

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components is underway while preferring

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checkout of the launch vehicle was

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underway modifications were completed on

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Apollo boiler plate number 9 the service

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module and adapter were shipped from

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Marshall to the Cape June 20th the

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command module and launch escape system

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were shipped on June 29th following

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mating with Pegasus boiler plate number

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nine will be erected atop the launch

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vehicle early next quarter Pegasus e

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electronic canister and thermal vacuum

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testing was completed at Bladensburg

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Maryland May 26 the satellite was then

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shipped to Fairchild Hiller's Hagerstown

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facility for final assembly and

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functional checkout

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Pegasus C were shipped to KSC June 22nd

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where it will receive pre-launch check

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out prior to mating with boiler plate

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number nine the launch of Pegasus II and

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sa 10 is scheduled for early next

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quarter at Marshall Saturn 1b dynamic

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testing of the complete vehicle

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configuration started last quarter was

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successfully completed May 27 no major

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problems were encountered during testing

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at the present time changeover is

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underway to the upper stage

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configuration which will allow

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simulation of s4

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be flight conditions following

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completion of change over next quarter

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dynamic testing will resume s1 bt has

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been shipped to the Michou assembly

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facility for storage and such

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modifications as necessary for the

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Saturn 1b sent our launch vehicle

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dynamic test program in April at

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Chrysler Michou a failure during the s1

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be structural testing revealed a spider

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beam marginal design MSFC and Chrysler

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investigated the failure resolved the

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problem and modified the beam on June

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19th the modified spider beam was

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successfully tested to the required 140

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percent load a major milestone in the

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Saturn 1b program was the static firing

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at Marshall of the first 1b booster on

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April 1st the booster built by Chrysler

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was successfully fired for a duration of

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35 seconds on April 13th and equally

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successful long duration firing was

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accomplished the stage was removed from

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the static test stand and transported to

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Marshalls loading docks on April 20th

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the stage departed MSFC and arrived at

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me Shu four days later following

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completion a post static modification

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post static checkout began June 11 the

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checkout will be completed in July the

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stage is scheduled to arrive at KSC in

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mid-august for use in the checkout of

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launch complex 34 prior to beginning

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pre-flight check also at Chrysler me Shu

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s1 b202 pre static checkout was

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completed April 22nd on May 21st

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installation of retrofitted engines was

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completed along with the necessary

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electrical tests and engine alignment

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the stage was then prepared for shipment

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to Marshall departing Mishu June 12th

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arriving at MSFC June 19

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s1b 202 is scheduled to be static fired

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early next quarter at Michou Chrysler

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completed Assembly of s 1 B 2 o 3 June

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16th following installation pre static

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checkout of the booster started June

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17th and continued throughout June on

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April 5th s1 b204 tank clustering began

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with completion in early June assembly

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operations on the booster will continue

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into August fabrication of s 1 B 2 O 5

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major structural components continued

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through the quarter on May 12th Assembly

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of the second stage adapter was begun

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with tank clustering scheduled for July

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12th fabrication operations for s1 B 206

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are also underway the lower thrust ring

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was completed on May 14th on June 28 the

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barrel assembly was completed stage

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fabrication will continue through next

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quarter at Rocketdyne Santa Susana

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facility 200k h1 engine qualification

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testing begun last quarter was completed

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April 30th the test program included

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functional and reliability tests of the

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locks valve turbo pump and thrust

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chamber 8 200k h1 engines will power the

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s-1 B stains another Saturn 1b major

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milestone was reached at sacto when the

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final 1b s4v battleship tests were

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performed during May on May 4th a

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successful full gimbal full duration

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firing was performed on May 14th

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successful environmental temperature

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conditioning tests were conducted these

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concluded the Saturn 1b battleship

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program conversion of the stage 2 Saturn

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5 configuration began immediately also

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at Sacramento the s4b facilities

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checkout stage underwent successful

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propellant loading tests at Douglass's

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beta test and number three this quarter

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qualifying both the stage and test and

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on May first automatic loading tests

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were successfully completed following

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testing the stage was removed from the

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stand and moved to an inspection site no

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discrepancies were revealed during

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post-test inspections of the propellant

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tanks lh2 tank insulation and dye checks

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of all exposed Wells the stage was

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subsequently prepared for shipment at

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Sacto and departed by a water

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transportation for KSC June 10th

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arriving June 30th the stage will be

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used in the checkout of launch complex

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34 construction of the vertical checkout

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laboratory at Sacto is well underway

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erection of structural steel is complete

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and installation of handling and test

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equipment is underway following

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acceptance the facility will be used for

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post static check out of s4v stages

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after acceptance firing a tear

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researchers test facility in Phoenix

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Arizona qualification testing of the

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fuel feed duct for s4b stages was

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conducted this quarter at Douglass's

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Huntington Beach facility the first s4b

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flight stage s4v 201 underwent lh2 tank

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modifications parts shortage

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installation painting and weighing the

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stage was then shipped to sacto April

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30th arriving May 6th the next day it

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was installed in beta test stand number

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3 we're out of position installations

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and modifications were begun pre static

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checkout began May 29th and continued

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through June a major milestone will be

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reached early next quarter with the

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acceptance firing of the first flight

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s4b stage major assembly on s4b 202 was

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completed April 30th checkout started

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the same day and continued through the

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quarter in parallel with installation of

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late parts s4b 203 clip bonding is now

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complete installations in the LH 2 tank

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and component installation in the

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forward and aft skirts and thrust

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structure continued installation of the

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LH 2 tanks for s4b 204 was completed in

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May

246
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installation of helium spheres in the

247
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lh2 tank was completed in late May in

248
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early May at santa monica s4b 205

249
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fabrication and assembly of the LOX tank

250
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was completed the LOX tank and lh2

251
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segments were then shipped to Huntington

252
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Beach joining of the lh2 and lox tanks

253
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occurred in mid-may joining of the

254
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forward dome was completed in early June

255
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lh2 insulation is scheduled for next

256
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quarter assembly of s4b 206 aft common

257
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bulkheads started May 4th work continued

258
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on the joining of aft and forward common

259
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bulkheads development and manufacturing

260
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of the s4 B's j2 engine continued

261
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throughout the quarter at status suzana

262
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modifications to rocky tines vertical

263
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stand 3a for j2 engine static tests

264
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started last quarter were completed in

265
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early June initial static firing

266
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occurred in mid April in order to

267
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improve manufacturing workload

268
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distribution Rocketdyne transferred the

269
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j2 liquid oxygen turbo pump fabrication

270
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from Canoga Park California to its

271
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Neosho Missouri plant as part of the

272
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flight rating test program which was

273
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successfully completed on June 30th six

274
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satisfactory malfunction tests were

275
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performed at Santa Susana this quarter

276
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during these tests malfunctions are

277
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deliberately phased into an engine to

278
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determine effect on performance and to

279
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see if a safe shutdown can be

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accomplished the other flight rating

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tests including altitude testing series

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safety limit series and malfunction

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series were successfully conducted with

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engines 2002 and 2003 at Marshall the

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first j2 engine delivered by Rocketdyne

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was installed in the static test and in

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April it is being used to familiarize

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MSFC personnel with the engine a second

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engine delivered to Marshall in June

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will be used to

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activate the stand at Wiley laboratories

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Huntsville instrument unit vibration

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testing started last quarter continued

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through April and May tests revealed

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deficiencies in the mounting of

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components to the IU structure

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consequently it was decided to bolt the

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mounting pads to the structure in

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addition to bonding additional vibration

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tests are underway to qualify the

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mechanically fastened mounting pads at

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Marshall assembly was completed in

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mid-june on the facilities check out

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instrument unit the unit was shipped

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from MSFC to Michou with s1 BD June 19th

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arriving June 23rd it will be

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temporarily stored then shipped to the

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Cape with s 1 B 201 for a launch complex

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34 check out instrument unit structural

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testing began May 27th at Marshall

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testing revealed a necessity for minor

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changes in the IU access door which have

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00:16:23,340 --> 00:16:21,760
been made to series of tests have been

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completed with the third and final

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series to be conducted early next

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quarter assembly of structural segments

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for the second I use structural test

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00:16:37,020 --> 00:16:34,480
unit began June 8 with completion

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scheduled in late July structural

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testing of this unit will verify the

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00:16:46,160 --> 00:16:41,110
segment's built by North American to be

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flown on si 203 and subsequent vehicles

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work continued on SIU 201 with

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installation of inserts to allow bolting

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00:16:57,030 --> 00:16:54,240
of all mounting pads to the structure

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component installation will be completed

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next quarter with checkout also

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00:17:03,270 --> 00:17:01,210
scheduled for next quarter component

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installation is also well underway on

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SIU 202 work is well underway at

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Marshall system development facility

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with installation of black boxes on IU

333
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simulator cold plates and scheduled

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00:17:18,510 --> 00:17:16,870
vehicle hardware check out the

335
00:17:22,770 --> 00:17:18,520
breadboard is expected to be fully

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00:17:25,319 --> 00:17:22,780
operational by September meanwhile work

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00:17:27,110 --> 00:17:25,329
continues toward activation of IBM's I

338
00:17:30,900 --> 00:17:27,120
you check out station at Huntsville

339
00:17:32,790 --> 00:17:30,910
Atmos you ii up to s1 check out stations

340
00:17:35,310 --> 00:17:32,800
to be modified to the s-1 b

341
00:17:40,200 --> 00:17:35,320
configuration was completed in

342
00:17:42,360 --> 00:17:40,210
a summary of the Saturn one 1b program

343
00:17:49,230 --> 00:17:42,370
from April through the end of June shows

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major accomplishments in all areas the

345
00:18:07,230 --> 00:18:02,150
preparations for the flight of s 8n

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00:18:10,880 --> 00:18:07,240
Saturn 1b stage build-up acceleration of

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00:18:13,320 --> 00:18:10,890
events within the j2 engine program and

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00:18:16,710 --> 00:18:13,330
continued buildup of ground support

349
00:18:18,960 --> 00:18:16,720
equipment during the next report period

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00:18:21,180 --> 00:18:18,970
additional major milestones will be

351
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reached strengthening the established