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perience Report because in his judgment the use of SI units would impair the usefulness of
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150 Pressure 5K PSIA Accelerometer Apollo 11 Apollo Program Caution and warning Central timing equipment checkout procedures command and service communications subsystem contractor and NASA corrective action data pack Data storage equipment data users Differential amplifier Differential pressure transducer Electromagnetic interference equipment 45 flight failures FLIGHT LEVEL TEMPERATURES FLIGHT LEVELS FNG BANK ground station implementation instrumentation engineer instrumentation equipment list instrumentation hardware Johnson Space Center junction box Mass-flow transducer measurement requirements list measurement system module instrumentation subsystem OEG F off-limits tests parameter PEG F personnel Power supply 65 Pressure transducer process specifications procurement specifications Propellant compatibility Pulse-code modulation QUALIFICATION TEST quality assurance Reference junction schematics service module instrumentation SERVICE PROPULSION SYSTEM shown in figure Signal conditioning equipment specification control drawing subsystem manager telemetry interface TEMP temperature ratio transducer Temperature transducer TESTS AND FLIGHT Thermocouple transducers and signal type of measurement very-high-frequency VLV 1 POT voltage wiring diagram X X X