SPACE LAUNCH REPORT CZ-12A Launch Vehicle Flight History by Variant/Year (1957-Present) by: Ed Kyle, Last Update December 24, 2025 L(F) = Number of Launches(Number of Failures) CZ-12A Year L(F) L(F) L(F) L(F) L(F) L(F) L(F) L(F) ------------------------------------------------------------------ 2025 1(0) ------------------------------------------------------------------ CZ-12A L(F) L(F) L(F) L(F) L(F) L(F) L(F) L(F) ------------------------------------------------------------------ Suborb - - - - - - - - Orbit 1(0) Totals 1(0) ------------------------------------------------------------------ Footnotes: "CZ" = Chang Zheng (Long March) CZ-12A = A Methane/LOX 2-stage rocket using 3.8 m diameter tanks. Began flying from new commercial pad at Jiquan in 2025. First stage is designed to reenter and land downrange. CZ-12A Vehicle Configuration ------------------------------------------------------------------ LEO GTO Height GLOW (tonnes) (tonnes) (meters) (tonnes) [1] LEO reuse [2] SSO reuse [3] LEO expend ================================================================== CZ-12 (2-stg) 6 t[1] 70.4 m 437 t 3 t[2] 9 t[3] ================================================================== ================================================================== CZ-12A Vehicle Components ------------------------------------------------------------------ 3.8 m 3.8 m 4.2 5.2 m Stg 1 Stg 2 PLF PLF ================================================================== Dia (m) 3.8 m 3.8 m 4.2 m 5.2 m Len (m) m m m m Mb/o (t) t t t t Mp(t) t t GLOW (t) t t Engine 7x 1xYF209V Longyun 70 Mfgr Fuel Methane Methane Oxidizer LOX LOX T(SL t) T(Vac t) 525 t 96 t ISP(SL s) ISP(Vac s) Tburn (s) No. Eng 7 ` ================================================================== CZ-12A LAUNCH HISTORY DATE VEHICLE ID PAYLOAD MASS(t) SITE ORBIT ------------------------------------------------------------------ 12/23/25 CZ-12A Y1 Demo, 2 objects JQ DC1 LEO ------------------------------------------------------------------ [CZ12A-Y1] 12/23/25 0200. Demo launch from new Dongfeng Commercial Space Innovation Test Zone at Jiuquan. Successfully reach LEO, with 2 object tracked in 203 x 241 km x 69.71 deg. First stage downrange landing attempt failed. One of three planned engines failed during entry burn. Stage plummeted to impact. JQ = Jiquan, China DC1 = Dongfeng Commercial Space Innovation Test Zone, Pad 1 40.891 N, 100.217 E LEO - Low Earth Orbit SSO - Sun Synchronous Orbit CSS - China Space Station orbit GTO - Geosynchronous Transfer Orbit GEO - Geosynchronous Orbit TLI - Trans Lunar Orbit HCO - Heliocentric Orbit [FTO] - Failed to Orbit CZ-12A LAUNCH VEHICLE by Ed Kyle CZ-12A is a 3.8 m diameter, two-stage, LOX/methane-fueled launch vehicle. It uses seven Longyun 70 first stage engines and a single YF209V second stage engine. The first stage is designed to reenter and land downrange. This is facilitated by restartable engines designed to perform entry and landing burns, along with four steering grid fins and four deployable landing legs. References Jonathan's Space Report Launch Vehicle Database "http://www.planet4589.org/space/lvdb/index.html" Encylopedia Astronautica "http://www.astronautix.com/" Gunter's Space Page "http://www.skyrocket.de/space"