File:Crews Complete SLS Liquid Oxygen Tank Forward Dome for Artemis IV (MAF 20230711 CS4 LoxFwdDomeLift10).jpg

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	Date/Time	Thumbnail	Dimensions	User	Comment
current	01:20, 24 July 2023		7,164 × 4,778 (22.22 MB)	commons>OptimusPrimeBot	#Spacemedia - Upload of http://images-assets.nasa.gov/image/MAF_20230711_CS4_LoxFwdDomeLift10/MAF_20230711_CS4_LoxFwdDomeLift10~orig.jpg via Commons:Spacemedia

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Camera manufacturer	Canon
Camera model	Canon EOS R5
Exposure time	1/800 sec (0.00125)
F Number	f/2.8
ISO speed rating	1,600
Date and time of data generation	13:46, 11 July 2023
Lens focal length	23 mm
City shown	New Orleans
Short title	Crews Complete SLS Liquid Oxygen Tank Forward Dome for Artemis IV
Author	Michael DeMocker
Image title	Teams completed welding of the liquid oxygen dome for the core stage of a future SLS (Space Launch System) rocket at NASA’s Michoud Assembly Facility in New Orleans. The dome, which will cap off the forward end of the liquid oxygen tank, was lifted off of the robotic weld tool and moved to an assembly area for the next phase of production. Later, crews will add the forward dome to join the two barrels and the aft dome to complete the liquid oxygen tank. The flight hardware will be used for Artemis IV, the first flight of SLS in its Block 1B configuration. The SLS core stage liquid oxygen tank holds 196,000 gallons of super-cooled liquid propellant. The SLS core stage is made up of five unique elements: the forward skirt, liquid oxygen tank, intertank, liquid hydrogen tank, and the engine section. The liquid oxygen and the liquid hydrogen tanks will provide propellant to the four RS-25 engines to produce more than two million pounds of thrust to help launch NASA’s Orion spacecraft, astronauts, and supplies beyond Earth’s orbit to the Moon. Image credit: NASA/Michael DeMocker
Copyright holder	(NASA/MAF) For copyright and restrictions refer to - http://www.nasa.gov/multimedia/guidelines/index.html
Width	8,192 px
Height	5,464 px
Bits per component	8 8 8
Pixel composition	RGB
Orientation	Normal
Number of components	3
Horizontal resolution	300 dpi
Vertical resolution	300 dpi
Software used	Adobe Photoshop 24.6 (Macintosh)
File change date and time	09:08, 23 July 2023
Y and C positioning	Co-sited
Exposure Program	Aperture priority
Exif version	2.31
Date and time of digitizing	13:46, 11 July 2023
Meaning of each component	Y Cb Cr does not exist
APEX shutter speed	9.625
APEX aperture	3
APEX exposure bias	0
Maximum land aperture	3 APEX (f/2.83)
Metering mode	Pattern
Flash	Flash did not fire
DateTime subseconds	52
DateTimeOriginal subseconds	52
DateTimeDigitized subseconds	52
Supported Flashpix version	1
Color space	sRGB
Focal plane X resolution	5,773.0796335447
Focal plane Y resolution	5,769.7993664203
Focal plane resolution unit	inches
Custom image processing	Normal process
Exposure mode	Auto exposure
White balance	Auto white balance
Scene capture type	Standard
GPS tag version	0.0.3.2
IIM version	3
Province or state shown	LA
Country shown	USA
Keywords	SLS MAF Michoud Assembly Facility MSFC Marshall Space Flight Center Artemis IV Artemis Space Launch System Louisiana Mars Moon NASA New Orleans LOX Liquid Oxygen Tank Core Stage
Sublocation of city shown	NASA Michoud Assembly Facility
Serial number of camera	052021002160
Lens used	RF15-35mm F2.8 L IS USM
Date metadata was last modified	04:08, 23 July 2023
Rating (out of 5)	0
Unique ID of original document	0DF856152410D57C8139D018B82D13B1
Copyright status	Copyrighted

File:Crews Complete SLS Liquid Oxygen Tank Forward Dome for Artemis IV (MAF 20230711 CS4 LoxFwdDomeLift10).jpg

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