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DESIGN USING EXISTING TECHNOLOGY
TEST EQUIPMENT DESIGN
2 other sections not shown
28 V dc accelerometers antenna Apollo 4 mission Apollo Program attitude control attitude indicator automatic backup breadboard bus A safe certification checkout equipment circuitry components connector control assembly delay delivery filter capacitors Flotation functional test G&N system computer gimbal motor Ground command controller grounds G hardware input keying commands latching relays launch vehicle Lift-off logic MCP design MCP redundancy test MCP system megohm test MESC mission control programer mission events MISSION SEQUENCE MISSIONS AS-202 NASA NOMINAL MISSION operation performed pins postenvironmental Printed wiring board problem pulse qualification test redundant paths relay drivers reorientation Reset real-time command S-band S-IVB SCC unit schedule sec MCP SEQUENCE OF EVENTS signal SM quad solder solder-closeout relays spacecraft 017 Spacecraft command controller spacecraft Oil spacecraft systems spacecraft test switch test equipment test tape time-delay circuits time-delay failures transistors unmanned flights updata link verified very-high-frequency wiring zener diode