File:S-IV rocket stage.jpg

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Summary

Description
English: This cutaway of the Saturn I S-IV stage (second stage) illustrates the booster's components. Powered by six RL-10 engines, the S-IV stage was capable of producing 90,000 pounds of thrust. Development of the Saturn S-IV stage by the Marshall Space Flight Center (MSFC) contributed many technological breakthroughs vital to the success of the Apollo lunar program, including the use of liquid hydrogen as a propellant.
Date
Source https://images.nasa.gov/details-9801758 (image link)
Author NASA/MSFC
This image or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: 9801758.

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This image or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: MSFC-MS-G-87-4-63.

This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing.

Licensing

Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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  • 2004-06-10 05:07 Reubenbarton 640×480× (84202 bytes) S-IV Saturn I rocket second stage

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15 September 1963

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Date/TimeThumbnailDimensionsUserComment
current15:36, 22 March 2020Thumbnail for version as of 15:36, 22 March 20201,137 × 852 (778 KB)HuntsterHigher resolution version.
12:40, 26 December 2008Thumbnail for version as of 12:40, 26 December 2008640 × 480 (82 KB)File Upload Bot (Magnus Manske) {{BotMoveToCommons|en.wikipedia}} {{Information |Description={{en|S-IV Saturn I rocket second stage Downloaded from the NASA Marshall Spaceflight Center Image (MIX) Exchange Serve: http://mix.msfc.nasa.gov/abstracts.php?p=1530}} |Source=Transferred fro
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