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The Saturn V Instrument Unit is a ring-shaped structure fitted to the top of the Saturn V rocket's third stage (S-IVB) and the Saturn IB's second stage (also an S-IVB). It was immediately below the SLA ''(Spacecraft/Lunar Module Adapter)'' panels that contained the Lunar Module. The Instrument Unit contains the guidance system for the Saturn V rocket. Some of the electronics contained within the Instrument Unit are a digital computer, analog flight control computer, emergency detection system, inertial guidance platform, control accelerometers and control rate gyros. The instrument unit (IU) for Saturn V was designed by NASA at Marshall Space Flight Center (MSFC) and was developed from the Saturn I IU.〔"Instrument Unit Fact Sheet, Saturn V News Reference." Changed December 1968. Page 2.〕 NASA's contractor to construct the Saturn V Instrument Unit was International Business Machines (IBM).〔Roger E. Bilstein. ''Stages to Saturn''. The NASA History Series, 1996. Chapter 8. From Checkout to Launch: The Quintessential Computer. IBM is also identified as the Instrument Unit builder on the nameplate of IU-514 at Udvar-Hazy Center. This nameplate is at the top left of location 7.〕 One of the unused Instrument Units is currently on display at the Steven F. Udvar-Hazy Center in Chantilly, Virginia. The plaque for the Unit has the following inscription:
==Instrument Unit specifications== *Diameter: 260 inches (6.6 m) *Height: 36 inches (914 mm) *Weight at launch: ~4,400 lb (1996 kg) 抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Saturn V Instrument Unit」の詳細全文を読む スポンサード リンク
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