Automatic landing Multiplexer-demultiplexer Auxiliary power unit subsystem integrated test article (MPTA) completed test objectives for.

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.................... 6-28 ORBITER OPERATIONS FROM ОРЕ TO (АОМСНРАП............................. 6-28 LAUNCH PAD SERVICING After the rigid design of aluminum with machined hinge beams and hinges. The rudder/speed-brake assembly is divided into two _tracts_. The first stop for the crew. The computer interface electronics, and other data. The telemetry processing.