File:Crews Complete SLS Liquid Oxygen Tank Forward Dome for Artemis IV (MAF 20230711 CS4 LoxFwdDomeLift10).jpg
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Size of this preview: 800 × 534 pixels. Other resolutions: 320 × 213 pixels | 640 × 427 pixels | 1,024 × 683 pixels | 1,280 × 854 pixels | 2,560 × 1,707 pixels | 7,164 × 4,778 pixels.
Original file (7,164 × 4,778 pixels, file size: 22.22 MB, MIME type: image/jpeg)
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Summary
DescriptionCrews Complete SLS Liquid Oxygen Tank Forward Dome for Artemis IV (MAF 20230711 CS4 LoxFwdDomeLift10).jpg |
English: 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 |
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Date | Taken on 11 July 2023 | ||
Source |
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Author | NASA Michoud Assembly Facility / Michael DeMocker |
Licensing
Public domainPublic domainfalsefalse |
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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image/jpeg
4,778 pixel
7,164 pixel
23,298,645 byte
aaa62838be8bafe17fad3a5e4c88fe970ef55ff9
11 July 2023
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 01:20, 24 July 2023 | 7,164 × 4,778 (22.22 MB) | 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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Metadata
This file contains additional information, probably added from the digital camera or scanner used to create or digitize it.
If the file has been modified from its original state, some details may not fully reflect the modified file.
Camera manufacturer | Canon |
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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 |
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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 |
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Shutter speed | 9.625 |
APEX aperture | 3 |
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 |
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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 |