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File:SaturnV S-IVB.jpg

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English: This cutaway illustration shows the Saturn V S-IVB (third) stage with the callouts of its major components. When the S-II (second) stage of the powerful Saturn V rocket burnt out and was separated the remaining units approached orbit around the Earth. Injection into the desired orbit was attained as the S-IVB (third stage) was ignited and burnt. The S-IVB stage was powered by a single 200,000-pound thrust J-2 engine and had a re-start capability built in for its J-2 engine. The S-IVB restarted to speed the Apollo spacecraft to escape velocity injecting it and the astronauts into a moon trajectory.
Date circa 1967
date QS:P,+1967-00-00T00:00:00Z/9,P1480,Q5727902
Source https://images.nasa.gov/details-0100983
Author NASA
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-0100983.

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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-67-IND-1200-65 A.

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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Date/TimeThumbnailDimensionsUserComment
current16:11, 21 March 2020Thumbnail for version as of 16:11, 21 March 20203,000 × 2,231 (6.03 MB)HuntsterLess compression.
14:46, 21 March 2020Thumbnail for version as of 14:46, 21 March 20203,000 × 2,231 (1.13 MB)HuntsterHigher resolution.
15:27, 5 December 2005Thumbnail for version as of 15:27, 5 December 2005720 × 535 (103 KB)Maldoror~commonswikiSaturn V S-IVB (Third) Stage. (NASA illustration) "This cutaway illustration shows the Saturn V S-IVB (third) stage with the callouts of its major components. When the S-II (second) stage of the powerful Saturn V rocket burnt out and was separated the re

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