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

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<strong>Explor<strong>in</strong>g</strong> <strong>the</strong> <strong>Unknown</strong> 361<br />

Armstrong:<br />

Shortly after back<strong>in</strong>g off, we noticed that we were essentially los<strong>in</strong>g control<br />

of <strong>the</strong> spacecraft <strong>in</strong> roll and yaw and we suspected that we were over<br />

<strong>the</strong> life-time of <strong>the</strong>se attitude thrusters. <strong>The</strong> spacecraft was cont<strong>in</strong>u<strong>in</strong>g,<br />

however, to accelerate, and we were obta<strong>in</strong><strong>in</strong>g rates <strong>in</strong> roll at least that<br />

approached 200 to 300 degrees per second, or perhaps more.<br />

Scott:<br />

Yes, I would agree with that. It looked like even more to me, and it was by<br />

far more <strong>in</strong> roll than <strong>in</strong> yaw. <strong>The</strong> roll was <strong>the</strong> most predom<strong>in</strong>ate.<br />

Armstrong:<br />

We realized that physiological limits were be<strong>in</strong>g approached, and that we<br />

were go<strong>in</strong>g to have to do someth<strong>in</strong>g immediately, <strong>in</strong> order to salvage <strong>the</strong><br />

situation. So, we turned off all <strong>the</strong> OAMS thruster circuit breakers, closed<br />

<strong>the</strong> Attitude Control Power Switch, [61] closed <strong>the</strong> Motor Valves, armed<br />

<strong>the</strong> RCS, had no effect us<strong>in</strong>g <strong>the</strong> ACME, and went to DIRECT.<br />

Scott:<br />

I might add <strong>in</strong> <strong>the</strong>re that <strong>the</strong> rates were high enough that both of us had<br />

trouble see<strong>in</strong>g <strong>the</strong> overhead panel due to <strong>the</strong> vertigo problems and <strong>the</strong><br />

centrifugal force as we went around.<br />

Armstrong:<br />

<strong>The</strong> RCS DIRECT DIRECT was work<strong>in</strong>g satisfactorily and as soon as we<br />

determ<strong>in</strong>ed that we were able to reduce <strong>the</strong> rates us<strong>in</strong>g this mode, we<br />

turned <strong>the</strong> A-R<strong>in</strong>g OFF and reduced <strong>the</strong> rates slowly with <strong>the</strong> B-R<strong>in</strong>g,<br />

putt<strong>in</strong>g <strong>in</strong> a pulse to reduce <strong>the</strong> rate, <strong>the</strong>n wait<strong>in</strong>g awhile, <strong>the</strong>n putt<strong>in</strong>g <strong>in</strong><br />

ano<strong>the</strong>r pulse, and so on until <strong>the</strong> rates were essentially zero <strong>in</strong> all areas.<br />

At this time we carefully reactivated <strong>the</strong> OAMS, found some popped or<br />

<strong>in</strong>advertently manually actuated circuit breakers, OAMS control and so<br />

forth. Upon reactivat<strong>in</strong>g <strong>the</strong> system we found that <strong>the</strong> Number 8 thruster<br />

was failed on, so we left that circuit breaker off. We had no o<strong>the</strong>r yaw<br />

thrusters with <strong>the</strong> exception of Number 8 but <strong>the</strong> pitch was apparently<br />

start<strong>in</strong>g to come back <strong>in</strong> and we ensured that <strong>the</strong> roll logic was <strong>in</strong> pitch.<br />

We stayed <strong>in</strong> PULSE, controll<strong>in</strong>g <strong>the</strong> spacecraft with pitch and roll pulses<br />

<strong>the</strong>n to essentially a BEF attitude. [62]<br />

Scott:<br />

Do you want to add <strong>in</strong> <strong>the</strong>re about <strong>the</strong> hand controller, <strong>in</strong> not gett<strong>in</strong>g<br />

anyth<strong>in</strong>g?<br />

Armstrong:<br />

Yes. When I earlier referred to <strong>the</strong> fact that I’d lost control completely it<br />

appeared to us as though at that time we had no control out of <strong>the</strong> hand<br />

controller <strong>in</strong> any axis. I might reiterate that we reactivated <strong>the</strong> OAMS and<br />

found no roll or yaw control with <strong>the</strong> Number 8 circuit breaker off but<br />

pitch was slowly com<strong>in</strong>g back <strong>the</strong>n. It was somewhat <strong>in</strong>effective at first,<br />

but it was usable after awhile. Sometime later we saw <strong>the</strong> Agena, approxi-

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