{"id":507231,"date":"2023-09-13T13:45:09","date_gmt":"2023-09-13T17:45:09","guid":{"rendered":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg"},"modified":"2023-10-17T16:26:53","modified_gmt":"2023-10-17T20:26:53","slug":"sls-4533-icps-infographic6-2","status":"inherit","type":"attachment","link":"https:\/\/www.nasa.gov\/image-detail\/sls-4533-icps-infographic6-2\/","title":{"rendered":"NASA\u2019s SLS Mega Rocket: What Is the ICPS?"},"author":35,"comment_status":"closed","ping_status":"closed","template":"","meta":{"nasa_hds_core_meta_l10n":"en-US","nasa_hds_core_meta_article_editor":"","nasa_hds_core_meta_article_contacts":[],"nasa_hds_core_meta_article_topic":"","nasa_hds_core_meta_linked_locations":[],"nasa_hds_core_meta_article_related_articles":[],"hds_migrate_meta_pr_release_id":"","hds_migrate_meta_pr_release_type":"","nasa_hds_core_meta_location_x":"","nasa_hds_core_meta_location_y":"","nasa_hds_core_meta_gallery_images":[],"nasa_hds_core_meta_video_cc_file_id":"","nasa_hds_core_meta_audio_cc_file_id":""},"media-tags":[1468],"read_time":1,"video_cc_url":"","audio_cc_url":"","credits":"NASA\/Kevin O\u2019Brien","original_date":{"stamp":1693526400,"display":"September 1st, 2023"},"description":{"rendered":"<p class=\"attachment\"><a href='https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg'><img loading=\"lazy\" decoding=\"async\" width=\"300\" height=\"225\" src=\"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=300\" class=\"attachment-medium size-medium\" 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.\" srcset=\"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg 2681w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=300,225 300w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=768,576 768w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=1024,768 1024w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=1536,1152 1536w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=2048,1536 2048w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=400,300 400w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=600,450 600w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=900,675 900w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=1200,900 1200w, https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?resize=2000,1500 2000w\" sizes=\"(max-width: 300px) 100vw, 300px\" \/><\/a><\/p>\n<p>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. <\/p>\n"},"caption":{"rendered":"<p>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. <\/p>\n"},"alt_text":"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.","media_type":"image","mime_type":"image\/jpeg","media_details":{"width":2681,"height":2011,"file":"2023\/09\/sls-4533-icps-infographic6.jpg","filesize":2901598,"sizes":{"thumbnail":{"file":"sls-4533-icps-infographic6.jpg?resize=150,150","width":150,"height":150,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=150&h=150&crop=1"},"medium":{"file":"sls-4533-icps-infographic6.jpg?resize=300,225","width":300,"height":225,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=300"},"medium_large":{"file":"sls-4533-icps-infographic6.jpg?resize=768,576","width":768,"height":576,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=1024"},"large":{"file":"sls-4533-icps-infographic6.jpg?resize=1024,768","width":1024,"height":768,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=1024"},"1536x1536":{"file":"sls-4533-icps-infographic6.jpg?resize=1536,1152","width":1536,"height":1152,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=1536"},"2048x2048":{"file":"sls-4533-icps-infographic6.jpg?resize=2048,1536","width":2048,"height":1536,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=2048"},"thumbnail-sm":{"file":"sls-4533-icps-infographic6.jpg?resize=50,50","width":50,"height":50,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=50&h=50&crop=1"},"thumbnail-md":{"file":"sls-4533-icps-infographic6.jpg?resize=100,100","width":100,"height":100,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=100&h=100&crop=1"},"thumbnail-lg":{"file":"sls-4533-icps-infographic6.jpg?resize=200,200","width":200,"height":200,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=200&h=200&crop=1"},"card-xsm":{"file":"sls-4533-icps-infographic6.jpg?resize=400,300","width":400,"height":300,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=400"},"card-sm":{"file":"sls-4533-icps-infographic6.jpg?resize=600,450","width":600,"height":450,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=600"},"card-md":{"file":"sls-4533-icps-infographic6.jpg?resize=900,675","width":900,"height":675,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=900"},"card-lg":{"file":"sls-4533-icps-infographic6.jpg?resize=1200,900","width":1200,"height":900,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=1200"},"fullwidth":{"file":"sls-4533-icps-infographic6.jpg?resize=2000,1500","width":2000,"height":1500,"filesize":2901598,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg?w=2000"},"full":{"file":"sls-4533-icps-infographic6.jpg","width":1024,"height":768,"mime_type":"image\/jpeg","source_url":"https:\/\/www.nasa.gov\/wp-content\/uploads\/2023\/09\/sls-4533-icps-infographic6.jpg"}},"image_meta":{"aperture":"0","credit":"","camera":"","caption":"","created_timestamp":"0","copyright":"","focal_length":"0","iso":"0","shutter_speed":"0","title":"","orientation":"1","keywords":[]},"credits":"NASA\/Kevin 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