B J Funderburk; George C. Marshall Space Flight Center's Automation in Saturn I first stage checkout PDF

By B J Funderburk; George C. Marshall Space Flight Center

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Subcarrier oscillator frequency, deviation, stability linearity, and pre-emphasis . j. Multicoupler efficiency. All parameters, as a minimum, listed above are measured (eiher manually o r automatically) while the TLM system is operating in the stage network in as near a flight configuration as possible. These measurements are compared with measurements obtained previously in the functional bench check to determine trends and for compliance with applicable specifications. Calibration of subcarrier oscillators are checked and adjusted as necessary .

Hydraulic Systems. The objectives of this test are to check hydraulic systems f o r proper response, and system integrity. Each engine is gimbaled to verify structural clearance and proper travel. n. Instrument Canister and Cooling System. The objectives of this test are to check structural integrity, external leakage, components for internal leakage, and operation of cooling system components. _ Malfunction _ _ ~ ~Tests. _ _ The _ objectives of this test 4. General Network~ and are to verify overall design, function, and compatibility of the various cutoff sequences and verify proper operation and compatibility of the power transfer circuits, launch sequencer, and flight sequencer.

The operation of the DEE-3 is closely directed by the equipment operator. During the initialization of a test procedure, a special program-preparation phase allows the equipment operator to specify various operating modes. During this phase, the operator names the input lines which w i l l be used in the test. The number of input lines is also variable and is set at this time. During the actual events evaluation run, the equipment operator has several control features available. These take the form of special functions that the operator may request by keying them into the DEE-3A via the input typewriter.

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Automation in Saturn I first stage checkout by B J Funderburk; George C. Marshall Space Flight Center


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