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The global launch market reached $14.1 billion in 2024 — up 34% since 2021.
| Attribute | |||
|---|---|---|---|
| Company | LandSpace | CASC / CALT | Avio |
| Country | 🇨🇳 China | 🇨🇳 China | 🇪🇺 Europe |
| Status | Active | Active | In Development |
| Vehicle class | Medium | Heavy | Small |
| Propellant | CH₄ / LOX (9× TQ-12B first stage; TQ-15B vacuum upper stage) | UDMH/N₂O₄ (stages 1–2) + LH₂/LOX (stage 3 YF-75) | Solid (P160C first stage) / LOX-methane (cryogenic upper stage) |
| Reusable | Yes | No | No |
| Stages | 2 | 3 | 3 |
| First flight | 2025 | 1996 | 2027 |
| Payload to LEO | 21,000 kgas of [1]Expendable; ~18,300 kg with first-stage recovery ↑ Best | 11,200 kgas of [1] | — |
| Payload to GTO | — | 5,500 kgas of [1]With 4 strap-on liquid boosters (CZ-3B/E enhanced variant) ↑ Best | — |
| Height | 76.2 mas of [1] ↑ Best | 54.84 mas of [1] | — |
| Liftoff mass | ~660 tas of [1] ↑ Best | 426 tas of [1]Enhanced variant with 4 liquid strap-on boosters | — |
| Success rate | 100%as of [2]1/1 orbital successes (Y1, Dec 3, 2025). First-stage recovery failed — abnormal combustion during the landing burn crashed the booster near the landing zone. ↑ Best | ~95%as of [2]~6 failures/partial failures out of ~105+ flights; gradually being superseded by Long March 5 for GTO | — |
| Total flights | 1as of [3]Second orbital launch and recovery attempt targeted Q2 2026 per LandSpace | ~105as of [2] ↑ Best | — |
| Cost / kg LEO | — | — | — |
| Summary | LandSpace's stainless-steel, reusable methalox rocket — China's closest analogue to Falcon 9. The Y1 debut (Dec 3, 2025) reached orbit on the first attempt but lost the booster during its landing attempt; a second flight with another recovery attempt is targeted for Q2 2026. | China's primary geostationary transfer vehicle for over 25 years. Launched communications, meteorology, and navigation satellites including Beidou-3 (GEO/IGSO nodes). Being phased out in favour of Long March 5 for heavier GTO payloads as newer domestic communications satellites grow in mass. | The next evolution of ESA's Vega line: replaces the Zefiro-9 and AVUM+ stages with a single cryogenic LOX/methane upper stage powered by the new M10 engine, adding multi-orbit deployment flexibility. First flight is a stated target (2027), not yet flown. |
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.