{"id":25353,"date":"2026-06-20T17:09:10","date_gmt":"2026-06-20T09:09:10","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/detailed-comparison-of-rockets-currently-in-service-that-have-been-used-to-build-network-stars-for-starnet\/"},"modified":"2026-06-20T17:09:10","modified_gmt":"2026-06-20T09:09:10","slug":"detailed-comparison-of-rockets-currently-in-service-that-have-been-used-to-build-network-stars-for-starnet","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/detailed-comparison-of-rockets-currently-in-service-that-have-been-used-to-build-network-stars-for-starnet\/","title":{"rendered":"Detailed comparison of rockets currently in service that have been used to build network stars for StarNet"},"content":{"rendered":"<p>Rocket launch capability is the basic support and main constraint of satellite constellation networking, which directly determines the scale, cost and progress of constellation construction.<\/p>\n<p>Currently, StarNet has launched a total of 4 batches of network stars. Long March 5B launched twice, carrying 10 stars each time; Long March 8A launched once, carrying 9 stars at a time; Long March 6A launched once, carrying 5 stars at a time.<\/p>\n<p>Next, we will briefly review the various parameters of the Long March 5B, Long March 8A, and Long March 6A.<\/p>\n<p>1. Network overview<\/p>\n<p>rocket model<\/p>\n<p>Number of satellite launches<\/p>\n<p>Number of satellites built<\/p>\n<p>Long March 5B<\/p>\n<p>2<\/p>\n<p>10<\/p>\n<p>Long March No. 8A<\/p>\n<p>1<\/p>\n<p>9<\/p>\n<p>Long March No.6A<\/p>\n<p>1<\/p>\n<p>5<\/p>\n<p>2. Structural parameters<\/p>\n<p>rocket model<\/p>\n<p>Long March 5B<\/p>\n<p>Long March No. 8A<\/p>\n<p>Long March No.6A<\/p>\n<p>configuration<\/p>\n<p>Level one and a half<\/p>\n<p>Two and a half levels<\/p>\n<p>Two and a half levels<\/p>\n<p>core diameter<\/p>\n<p>5 meters<\/p>\n<p>3.35 meters<\/p>\n<p>3.35 meters<\/p>\n<p>boost diameter<\/p>\n<p>3.35 meters<\/p>\n<p>2.25 meters<\/p>\n<p>2 meters<\/p>\n<p>Number of boosters<\/p>\n<p>4<\/p>\n<p>2<\/p>\n<p>4<\/p>\n<p>Arrow body length<\/p>\n<p>53.657 meters<\/p>\n<p>50.539 meters<\/p>\n<p>50 meters<\/p>\n<p>quality<\/p>\n<p>849 tons<\/p>\n<p>371 tons<\/p>\n<p>530 tons<\/p>\n<p>3. Dynamic parameters<\/p>\n<p>(1) Boosting force<\/p>\n<p>rocket model<\/p>\n<p>Long March 5B<\/p>\n<p>Long March No. 8A<\/p>\n<p>Long March No.6A<\/p>\n<p>Booster type<\/p>\n<p>liquid boost<\/p>\n<p>liquid boost<\/p>\n<p>solid boost<\/p>\n<p>Number of boosters<\/p>\n<p>4<\/p>\n<p>2<\/p>\n<p>4<\/p>\n<p>Engine name<\/p>\n<p>YF-100<\/p>\n<p>YF-100<\/p>\n<p>FG-112<\/p>\n<p>Number of engines mounted on a single booster<\/p>\n<p>2<\/p>\n<p>1<\/p>\n<p>1<\/p>\n<p>propellant type<\/p>\n<p>liquid oxygen kerosene<\/p>\n<p>liquid oxygen kerosene<\/p>\n<p>Butylated hydroxyl<\/p>\n<p>Single engine thrust<\/p>\n<p>(sea level thrust)<\/p>\n<p>1223.5kN<\/p>\n<p>(124.8 tons)<\/p>\n<p>1223.5kN<\/p>\n<p>(124.8 tons)<\/p>\n<p>1214 kN<\/p>\n<p>sea \u200b\u200blevel specific impulse<\/p>\n<p>300 s<\/p>\n<p>300 s<\/p>\n<p>\/<\/p>\n<p>(2) One-level power<\/p>\n<p>rocket model<\/p>\n<p>Long March 5B<\/p>\n<p>Long March No. 8A<\/p>\n<p>Long March No.6A<\/p>\n<p>Engine name<\/p>\n<p>YF-77<\/p>\n<p>YF-100<\/p>\n<p>YF-100GAII<\/p>\n<p>Number of engines<\/p>\n<p>2<\/p>\n<p>2<\/p>\n<p>2<\/p>\n<p>propellant type<\/p>\n<p>liquid hydrogen liquid oxygen<\/p>\n<p>liquid oxygen kerosene<\/p>\n<p>liquid oxygen kerosene<\/p>\n<p>Single engine thrust<\/p>\n<p>(sea level thrust)<\/p>\n<p>518 kN<\/p>\n<p>1223.5kN<\/p>\n<p>(124.8 tons)<\/p>\n<p>1223.5kN<\/p>\n<p>(124.8 tons)<\/p>\n<p>sea \u200b\u200blevel specific impulse<\/p>\n<p>3106 m\/s<\/p>\n<p>300 s<\/p>\n<p>300 s<\/p>\n<p>(3) Second level<\/p>\n<p>rocket model<\/p>\n<p>Long March 5B<\/p>\n<p>Long March No. 8A<\/p>\n<p>Long March No.6A<\/p>\n<p>Engine name<\/p>\n<p>\/<\/p>\n<p>YF-75DA<\/p>\n<p>YF-115GIA<\/p>\n<p>Number of engines<\/p>\n<p>\/<\/p>\n<p>2<\/p>\n<p>1<\/p>\n<p>propellant type<\/p>\n<p>\/<\/p>\n<p>liquid hydrogen liquid oxygen<\/p>\n<p>liquid oxygen kerosene<\/p>\n<p>Single engine thrust<\/p>\n<p>(vacuum thrust)<\/p>\n<p>\/<\/p>\n<p>10 tons<\/p>\n<p>180 kN<\/p>\n<p>When performing the Starnet mission, Long March 5B is equipped with the Yuanzheng 2 upper stage. Yuanzheng-2 is my country\u2019s liquid-powered upper stage with the largest carrying capacity and strongest orbit-changing capability. Yuanzheng 2 is equipped with a YF-51D engine, which is composed of two YF-50D engines in parallel, with a total vacuum thrust of 13 kN. The propellant of YF-50D is dinitrogen tetroxide\/uniform dimethyl hydrazine, with a vacuum thrust of 6500 N and a vacuum specific impulse of 3099 m\/s.<\/p>\n<p>4. Performance parameters<\/p>\n<p>rocket model<\/p>\n<p>Long March 5B<\/p>\n<p>Long March No. 8A<\/p>\n<p>Long March No.6A<\/p>\n<p>LEO capacity<\/p>\n<p>>25 tons<\/p>\n<p>9.8 tons<\/p>\n<p>More than 8 tons<\/p>\n<p>SSO capacity<\/p>\n<p>>15 tons<\/p>\n<p>SSO (700 km): 7 tons<\/p>\n<p>SSO (900km): 6.8 tons<\/p>\n<p>SSO (500 km):>6.5 tons<\/p>\n<p>SSO (700 km):>5 tons<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Rocket launch capability is the basic support and main constraint of satellite constellation networking, which directly determines the scale, cost and progress of constellation construction. Currently, StarNet has launched a total of 4 batches of network stars. Long March 5B launched twice, carrying 10 stars each time; Long March 8A launched once, carrying 9 stars [&hellip;]<\/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-25353","post","type-post","status-publish","format-standard","hentry","category-news"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/25353"}],"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=25353"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/25353\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=25353"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=25353"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=25353"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}