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Exploring the Unknown: Selected Documents in ... - The Black Vault

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186<br />

First Steps <strong>in</strong>to Space: Projects Mercury and Gem<strong>in</strong>i<br />

subsequent cursory analysis of <strong>the</strong> systems showed that <strong>the</strong>re are several such. For<br />

example, three retro-rockets are provided to decelerate <strong>the</strong> capsule out of orbit.<br />

<strong>The</strong> entire package is held on by a s<strong>in</strong>gle explosive bolt. <strong>The</strong>re is a possibility that a<br />

stray current <strong>in</strong> <strong>the</strong> circuit beyond <strong>the</strong> ma<strong>in</strong> switch could fire <strong>the</strong> bolt prematurely<br />

and jettison <strong>the</strong> rocket package before it had performed its function and thus<br />

make it impossible to get out of orbit. Just such unexpla<strong>in</strong>ed currents have plagued<br />

two of <strong>the</strong> Little Joe shots. Ano<strong>the</strong>r possible difficulty centers around <strong>the</strong> necessity<br />

for releas<strong>in</strong>g both <strong>the</strong> ma<strong>in</strong> and <strong>the</strong> emergency parachutes from <strong>the</strong> capsule upon<br />

impact with <strong>the</strong> water. <strong>The</strong>re is a possibility that a premature spurious signal may<br />

make <strong>the</strong> release at high altitude and drop <strong>the</strong> capsule with catastrophic results.<br />

<strong>The</strong> panel is concerned that steps may not have been taken to specifically<br />

tabulate <strong>the</strong> operations or functions <strong>in</strong> which a signal failure would lead to<br />

catastrophe. When such possibilities have been def<strong>in</strong>ed, <strong>the</strong>n special test<strong>in</strong>g,<br />

<strong>in</strong>spection, and check out procedures should be adopted <strong>in</strong> order to obta<strong>in</strong> <strong>the</strong><br />

maximum possible reliability for <strong>the</strong> associated components.<br />

6. Status of <strong>the</strong> Quantitative Reliability Studies<br />

<strong>The</strong> recommendation of <strong>the</strong> preced<strong>in</strong>g section that <strong>the</strong> s<strong>in</strong>gle failure<br />

possibilities be critically analyzed serves to emphasize <strong>the</strong> value which a<br />

reliability analysis has <strong>in</strong> a program of this magnitude and complexity. From<br />

<strong>the</strong> presentations, it was learned that <strong>the</strong> McDonnell Aircraft Corporation had<br />

performed an extensive failure mode analysis and that a separate reliability study<br />

had been <strong>in</strong>itiated at NASA Headquarters and, subsequently, had been transferred<br />

to <strong>the</strong> Space Task Group.<br />

Through a misunderstand<strong>in</strong>g, <strong>the</strong> questions which were asked by <strong>the</strong><br />

panel about <strong>the</strong> McDonnell study were deferred until later <strong>in</strong> <strong>the</strong> brief<strong>in</strong>g when<br />

<strong>the</strong> reliability studies would be presented <strong>in</strong> detail. <strong>The</strong> later presentation proved<br />

to be on <strong>the</strong> NASA study, and consequently, very little was learned about <strong>the</strong><br />

failure mode analysis studies of McDonnell. Hence, no evaluation of <strong>the</strong>ir impact<br />

on <strong>the</strong> program can be made. [12]<br />

When <strong>the</strong> NASA reliability studies were presented, it became apparent<br />

that as yet <strong>the</strong>y had not played an important role <strong>in</strong> <strong>the</strong> design. <strong>The</strong> mean time to<br />

failure of each component which was <strong>the</strong> basic parameter <strong>in</strong> <strong>the</strong> analysis did not<br />

reflect <strong>the</strong> changes which had been made to correct obvious early difficulties. <strong>The</strong><br />

results which are available from a reliability analysis for <strong>the</strong> Atlas orbit<strong>in</strong>g mission<br />

<strong>in</strong> which <strong>the</strong> man is assumed to play no role. <strong>The</strong> analysis was <strong>in</strong> <strong>the</strong> process of<br />

be<strong>in</strong>g revised and results would not be available until approximately July 1,1961.<br />

In view of this situation, <strong>the</strong> panel was left <strong>in</strong> doubt as to how comprehensive has<br />

been <strong>the</strong> analysis of <strong>the</strong> possibilities of s<strong>in</strong>gle mode failures, of simple correlated<br />

multiple failures, and of subtle failures <strong>in</strong> redundant subsystems which might<br />

preclude <strong>the</strong> use of ei<strong>the</strong>r subsystem for <strong>the</strong> Atlas shots.<br />

In view of this uncerta<strong>in</strong>ty, <strong>the</strong> panel wishes to express an op<strong>in</strong>ion that an<br />

emphasis be placed on hav<strong>in</strong>g <strong>the</strong> results of such a systematic analysis available<br />

prior to <strong>the</strong> first launch<strong>in</strong>gs of <strong>the</strong> manned Atlas vehicles. Fur<strong>the</strong>r, <strong>the</strong> panel

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