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| Attribute | Long March 8 (incl. 8A) 🇨🇳 China Trust: Operator-primaryⓘ Last verified Active · Last updated 2026-07-26Remove × | ||
|---|---|---|---|
| Company | China Academy of Launch Vehicle Technology (CALT) / CASC | JAXA / Mitsubishi Heavy Industries | CASC / SAST |
| Country | 🇨🇳 China | 🇯🇵 Japan | 🇨🇳 China |
| Status | Active | Retired | Active |
| Vehicle class | Medium | Medium | Medium |
| Propellant | RP-1 / LOX (stage 1); LH2/LOX (stage 2) | LH₂ / LOX (LE-7A first stage + LE-5B second stage) | UDMH / N₂O₄ (hypergolic all stages) |
| Reusable | No | No | No |
| Stages | 2 | 2 | 2 |
| First flight | 2020 | 2001 – 2025 | 1992 |
| Payload to LEO | 8,100 kgas of [1]5,000 kg to 700 km SSO (base); the enlarged-second-stage 8A variant (first flew 2025-02-11) lifts 7,000 kg to the same SSO reference orbit. | 10,000 kgas of [1]202 configuration (2 SRB-A3 solid strap-ons) ↑ Best | 3,500 kgas of [1]SSO capacity ~1,300 kg; standard LEO 3,500 kg |
| Payload to GTO | — | 4,100 kgas of [1]202 configuration ↑ Best | — |
| Height | 50.3 mas of [1] | 53 mas of [1] ↑ Best | 41.06 mas of [1] |
| Liftoff mass | 356 t (base); 371 t (8A)as of [1] ↑ Best | 285 tas of [1]202 configuration | 232 tas of [1] |
| Success rate | 100% (16/16 combined base + 8A)as of [1] ↑ Best | 98%as of [2]49/50 successes. Only failure: F6 (Nov 2003, MTSAT-1R lost due to SRB separation anomaly). Retired after Flight 50 (GOSAT-GW, Jun 28, 2025). | 98.7%as of [2]~77/78 successes; one known failure (CZ-2D Y7, Mar 1995 upper-stage anomaly) |
| Total flights | 16 (base + 8A combined)as of [1] ↑ Best | 50as of [2]50 flights from 2001–2025. H3 replaces it from 2024 onward. | ~78as of [2] |
| Cost / kg LEO | — | — | — |
| Summary | A two-stage medium-lift launcher originally designed with a reusable combined-booster-recovery concept in mind, though currently operational vehicles fly expendable. Exclusively from Wenchang. | Japan's flagship medium-lift rocket for 24 years, retiring after an exceptional 49/50 mission success record. Launched the SELENE lunar orbiter (2007), Akatsuki Venus probe (2010), Hayabusa2 (2014), SLIM lunar lander (2023), and the ALOS series Earth observation satellites. | China's most-used sun-synchronous and polar orbit workhorse for small-to-medium military and commercial Earth observation satellites. Launched from Jiuquan and Taiyuan. Uses storable hypergolic propellants for high launch-readiness but produces toxic exhaust. |
48 launch vehicles across 10 countries — active, retired, and in development — with primary-source citations from manufacturer user guides and agency press kits. Pure URL state: bookmark or share the link and the comparison reproduces exactly.