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Launch System Infographics","url":"https:\/\/www.nasa.gov\/gallery\/space-launch-system-infographics\/","mainEntityOfPage":{"@type":"WebPage","@id":"https:\/\/www.nasa.gov\/gallery\/space-launch-system-infographics\/"},"thumbnailUrl":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=150&h=150&crop=1","image":{"@type":"ImageObject","url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg"},"articleSection":"General","author":[{"@type":"Person","name":"Beth Ridgeway"},{"@type":"Person","name":"Lee Mohon"}],"creator":["Beth Ridgeway","Lee Mohon"],"publisher":{"@type":"Organization","name":"NASA","logo":"https:\/\/www.nasa.gov\/wp-content\/themes\/nasa\/assets\/images\/nasa-logo.svg"},"keywords":[],"dateCreated":"2023-03-09T21:27:32Z","datePublished":"2023-03-09T21:27:32Z","dateModified":"2023-10-24T14:41:24Z"},"rendered":"<meta name=\"parsely-title\" content=\"Space Launch System Infographics\" \/>\n<meta name=\"parsely-link\" content=\"https:\/\/www.nasa.gov\/gallery\/space-launch-system-infographics\/\" \/>\n<meta name=\"parsely-type\" content=\"index\" \/>\n<meta name=\"parsely-image-url\" content=\"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=150&h=150&crop=1\" \/>\n<meta name=\"parsely-pub-date\" content=\"2023-03-09T21:27:32Z\" \/>\n<meta name=\"parsely-section\" content=\"General\" \/>\n<meta name=\"parsely-author\" content=\"Beth Ridgeway\" \/>\n<meta name=\"parsely-author\" content=\"Lee Mohon\" \/>","tracker_url":"https:\/\/cdn.parsely.com\/keys\/nasa.gov\/p.js"},"read_time":null,"time_ago":"1 year","featured_image":{"id":507231,"file":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg","title":"NASA\u2019s SLS Mega Rocket: What Is the ICPS?","alt":"NASA\u2019s SLS (Space Launch System) rocket\u2019s ICPS (interim cryogenic propulsion stage), with its single RL10 engine, produces 24,750 pounds of thrust to provide in-space propulsion for the agency\u2019s Artemis II and III missions, the first crewed missions under Artemis. Like the mega rocket\u2019s core stage, the ICPS uses liquid hydrogen and liquid oxygen to power its RL10 engine, manufactured by Aerojet Rocketdyne, an L3Harris Technologies company. The ICPS is built by ULA (United Launch Alliance) and Boeing. In addition to providing in-space propulsion, the ICPS also contains avionics to fly the mission after core stage separation until NASA\u2019s Orion spacecraft separates from the ICPS to venture to the Moon.","caption":"NASA\u2019s SLS (Space Launch System) rocket\u2019s ICPS (interim cryogenic propulsion stage), with its single RL10 engine, produces 24,750 pounds of thrust to provide in-space propulsion for the agency\u2019s Artemis II and III missions, the first crewed missions under Artemis. Like the mega rocket\u2019s core stage, the ICPS uses liquid hydrogen and liquid oxygen to power its RL10 engine, manufactured by Aerojet Rocketdyne, an L3Harris Technologies company. The ICPS is built by ULA (United Launch Alliance) and Boeing. In addition to providing in-space propulsion, the ICPS also contains avionics to fly the mission after core stage separation until NASA\u2019s Orion spacecraft separates from the ICPS to venture to the Moon. 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