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ST-124-M3 inertial platform
The ST-124-M3 is a device for measuring acceleration and attitude of the Saturn V launch vehicle. It was carried by the Saturn V Instrument Unit, a , section of the Saturn V that fit between the third stage (S-IVB) and the Apollo spacecraft. Its nomenclature means "stable table" (ST) for use in the moon mission (M), and it has 3 gimbals.〔Newsbureau, The Bendix Corporation, "Globe-shaped platform keeps Apollo on target."〕
==Development==
It was number 124 in a series of similar devices, including the ST-120 (used in the Pershing missile), the ST-90 (used on the Jupiter and on early Saturn I flights), and the ST-80 (used in the Redstone). They are descendants of the LEV-3 of the German V-2 rocket.〔Stages To Saturn, Chapter 8〕 The ST-124 was designed by Marshall Space Flight Center and manufactured by Bendix Corporation, Eclipse-Pioneer Division, in Teterboro, NJ. It took 9 men 22 to 24 weeks to assemble an ST-124, and 70 percent of that time was spent installing about 3,000 wires.〔Newsbureau, The Bendix Corporation, "Globe-shaped platform keeps Apollo on target."〕
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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