Lêer: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.
Datum circa 1967
date QS:P,+1967-00-00T00:00:00Z/9,P1480,Q5727902
Bron https://images.nasa.gov/details-0100983
Outeur 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.

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

Lisensiëring

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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huidig16:11, 21 Maart 2020Duimnaelskets vir weergawe vanaf 16:11, 21 Maart 20203 000 × 2 231 (6,03 MG)HuntsterLess compression.
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15:27, 5 Desember 2005Duimnaelskets vir weergawe vanaf 15:27, 5 Desember 2005720 × 535 (103 KG)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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