1. Long March 8A sun-synchronous orbit payload (700 km): 7 tons <\/p>\n
Estimated first launch: December 2024<\/p>\n
2. Long March 9 Low-Earth orbit load: 100 tons (two-stage configuration recovery) Low-Earth orbit load: 150 tons (two-stage configuration not recovered) Low-Earth orbit load: 80 tons (two-stage fully reusable configuration) Earth-moon transfer orbit load: 35 tons (three-stage configuration recovery) Earth-moon transfer orbit load: 50 tons (three-stage configuration not recovered) <\/p>\n
Estimated first launch time: 2033 (the third-stage configuration will not be recovered)<\/p>\n
3. Long March 10 Low-Earth orbit load: 70 tons Earth-moon transfer orbit load: no less than 27 tons <\/p>\n
Estimated first launch time: around 2027<\/p>\n
4. Long March 12 Low-Earth orbit payload (300 km): not less than 10 tons Sun-synchronous orbit payload (700 km): not less than 6 tons <\/p>\n
Estimated first launch: August 2024<\/p>\n
5. Kuaizhou-1B (solid rocket) <\/p>\n
Sun-synchronous orbit payload (700 km): 250-300 kg<\/p>\n
6. Hyperbola 3 series (decoding Beijing Interstellar Glory Space Technology Co., Ltd., China\u2019s first private company to achieve rocket into orbit) (1) Hyperbola 3 Low Earth orbit load (200~400 km, 42\u00b0): 13.7 tons (not recovered) Low Earth orbit load (200~400 km, 42\u00b0): 8.6 tons (recovered under the route) Low Earth orbit load (200~400 km, 42\u00b0): 5.1 tons (return to the site for recovery) Sun-synchronous orbit payload (500 km): 10.4 tons (not recovered) Sun-synchronous orbit payload (500 km): 6.2 tons (recovered under the route) Estimated first launch time: the second half of 2025 (2) Hyperbola-3A Low-Earth orbit payload (200-400 km, 42\u00b0): 26.1 tons (not recovered) Low-Earth orbit load (200-400 km, 42\u00b0): 12.9 tons (recovered under route) Low-Earth orbit load (200-400 km, 42\u00b0): 9.5 tons (return to site for recovery) (2) Hyperbola No. 3B Low-Earth orbit load (200-400 km, 42\u00b0): 32.2 tons (not recovered) Low-Earth orbit load (200-400 km, 42\u00b0): 14.1 tons (recovered under route) <\/p>\n
Low Earth orbit payload (200-400 km, 42\u00b0): 12.4 tons (return to site for recovery)<\/p>\n
7. Tianlong-3 series (Decoding Beijing Tianbing Technology Co., Ltd., how private rocket companies can succeed at launch) (1) Tianlong-3 Low-Earth orbit payload (800 km, 90\u00b0): \u226510 tons (Jiuquan) Sun-synchronous orbit payload (500 km): 14 tons (2) Tianlong-3H Low-Earth orbit payload: 68 tons Sun-synchronous orbit payload (500 km): 42 tons (2) Tianlong-3M <\/p>\n
Low earth orbit payload: 5 tons<\/p>\n
8. Zhuque-3 (decoding how Blue Arrow Aerospace Technology Co., Ltd., the world’s first liquid oxygen methane rocket successfully entered orbit) Low-Earth orbit payload (450 km): 21.3 tons (not recovered) Low-Earth orbit payload (450 km): 18.3 tons (recycling in the flight area) Low-Earth orbit payload (450 km): 12.5 tons (return to site for recovery) <\/p>\n
Estimated first launch: 2025<\/p>\n","protected":false},"excerpt":{"rendered":"
1. Long March 8A sun-synchronous orbit payload (700 km): 7 tons Estimated first launch: December 2024 2. Long March 9 Low-Earth orbit load: 100 tons (two-stage configuration recovery) Low-Earth orbit load: 150 tons (two-stage configuration not recovered) Low-Earth orbit load: 80 tons (two-stage fully reusable configuration) Earth-moon transfer orbit load: 35 tons (three-stage configuration recovery) […]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[],"class_list":["post-25410","post","type-post","status-publish","format-standard","hentry","category-news"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/25410"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=25410"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/25410\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=25410"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=25410"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=25410"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}