Category:Saturn IB/V Instrument Unit

English: 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 (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. NASA's contractor to construct the Saturn V Instrument Unit was International Business Machines (IBM).
<nowiki>サターンV飛行制御装置; Saturn V műszeregység (IU); 農神5號運載火箭控制裝置單元; 農神5號運載火箭控制設備單元; Saturn V Instrument Unit; Saturn IB/V Instrument Unit; 農神5號運載火箭控制設備單元; 農神5號運載火箭控制設備單元; Saturn V instrument unit; equipaggiamento; Ausrüstung; raketin ohjausjärjestelmät sisältämä osa; instrumentation platform on Saturn V; équipement; Saturn V Instrument Unit</nowiki>
Saturn IB/V Instrument Unit 
instrumentation platform on Saturn V
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Mass
  • 1,934 kg (minimum, launch weight, Apollo 7)
  • 2,007 kg (average)
  • 2,196 kg (maximum, launch weight, Apollo 8)
Diameter
  • 6.6 m
Height
  • 0.914 m
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Wikidata Q7426817
BabelNet ID: 03576855n
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This category has the following 12 subcategories, out of 12 total.

Media in category "Saturn IB/V Instrument Unit"

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