长征九号
Family-level launch record combining canonical variants, historical missions, public cadence forecasts, and available payload performance specs.
Historical missions are grouped by actual launch year. Forecast cadence uses family-level launch-rate rows.
| Year | Historical missions | Forecast launches |
|---|---|---|
| 2026 | 0 | 2 |
| 2027 | 0 | 2 |
| 2028 | 0 | 2 |
| 2029 | 0 | 2 |
| 2030 | 0 | 2 |
| 2031 | 0 | 2 |
| 2032 | 0 | 2 |
| 2033 | 0 | 2 |
| 2034 | 0 | 4 |
| 2035 | 0 | 4 |
| 2036 | 0 | 4 |
| 2037 | 0 | 4 |
| 2038 | 0 | 4 |
| 2039 | 0 | 4 |
| 2040 | 0 | 4 |
| 2041 | 0 | 4 |
1 launch location represented.
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Long March 9 | LEO | 150,000 kg | Unknown | Unknown | China State Council Long March 9 |
Long March 9 | TLI | 50,000 kg | Unknown | Unknown | China State Council Long March 9 |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
No recent missionsNo launched missions are linked to variants in this family. | ||
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Long March 9 | Not stated | 0 | Development |
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2027 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2028 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2029 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2030 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2031 | Wenchang Space Launch Site | 2 | 10% | Editable low-confidence annual throughput seed. |
| 2032 | Wenchang Space Launch Site | 2 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2033 | Wenchang Space Launch Site | 2 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2034 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2035 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2036 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2037 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2038 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2039 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2040 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2041 | Wenchang Space Launch Site | 4 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume constellation deploymen...
The Long March 9 will be 93 m long and feature a 10-meter-diameter core.
The Long March 9 first stage will use four dual-nozzle 500-ton-thrust engines sometimes referred to as the YF-130.
The Long March 9 is designed to lift 140,000 kg to low Earth orbit (LEO) or 50,000 kg to trans-lunar injection.
The Long March 9 is in the research and development stage with a test launch planned for around 2030.
A concept for Chinese crewed lunar missions involves a Long March 5B launch of the crew spacecraft followed by LEO rendezvous and docking with a lunar stack launched by a future Long March 9.
A previous Chinese human lunar mission concept relied on the Long March 9 super-heavy-lift launcher with a 10-meter diameter that China aims to fly in 2028 and included an Earth-orbit rendezvous using a Long March 5B to loft the crew.
China is developing the Long March 9 super-heavy-lift launch vehicle capable of lifting 140 metric tons to low Earth orbit, 50 metric tons to Earth–Moon transfer orbit, and 44 metric tons to Earth–Mars transfer orbit.
A tentative lunar mission concept involves launching a spacecraft on Long March 9 followed by astronauts launching on the next-generation crew spacecraft atop Long March 5B to rendezvous and dock in low Earth orbit before translunar injection.
The Long March 9 super heavy-lift launcher is in early development with a first flight planned for 2028–2030.
CASC is developing the Long March 9 super-heavy-lift launch vehicle with a projected capability of lifting up to 140 metric tons to LEO.
CALT is studying a mission profile that would use the Long March 5B to launch a crewed spacecraft that would rendezvous in low Earth orbit with a lunar spacecraft stack launched by the Long March 9.
CALT has achieved breakthroughs related to 220-ton-thrust hydrolox engines for the Long March 9 project.
The Long March 9 is expected to produce close to 6,000,000 kg of thrust.
The Long March 9 will use four boosters each with a diameter of up to 5 m.
The Long March 9 would be able to launch components for a space-based solar power system.