引力二号
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 | 4 |
| 2028 | 0 | 6 |
| 2029 | 0 | 8 |
| 2030 | 0 | 8 |
| 2031 | 0 | 8 |
| 2032 | 0 | 8 |
| 2033 | 0 | 10 |
| 2034 | 0 | 10 |
| 2035 | 0 | 10 |
| 2036 | 0 | 10 |
| 2037 | 0 | 10 |
| 2038 | 0 | 10 |
| 2039 | 0 | 10 |
| 2040 | 0 | 10 |
| 2041 | 0 | 10 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Gravity-2 | LEO | 21,500 kg | Unknown | Unknown | Ars Technica Rocket Report |
Gravity-2 | SSO | 15,000 kg | 500 km | Unknown | Orienspace product page |
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 |
|---|---|---|---|
Gravity-2 | Not stated | 0 | Development |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Haiyang Eastern Spaceport | 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... |
| 2027 | Haiyang Eastern Spaceport | 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... |
| 2028 | Haiyang Eastern Spaceport | 6 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2029 | Haiyang Eastern Spaceport | 8 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2030 | Haiyang Eastern Spaceport | 8 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2031 | Haiyang Eastern Spaceport | 8 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
| 2032 | Haiyang Eastern Spaceport | 8 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 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 | Haiyang Eastern Spaceport | 10 | 22% | China launch cadence curve: active Long March/Gravity families scale from current low-confidence static defaults toward an analytically modeled high-volume con... |
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...
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...
Gravity-2 is designed to deliver 25,600 kg to low Earth orbit (LEO), 19,100 kg to a 500-kilometer sun-synchronous orbit (SSO), and 7,700 kg to geostationary transfer orbit (GTO).
Gravity-2’s first stage will use nine 100-ton-thrust Yuanli-85 gas-generator, variable-thrust kerosene engines and be supported by solid boosters.
Gravity-2 aims to operate at a similar price per kilogram as SpaceX’s Falcon 9.
Orienspace plans the first Gravity-2 launch for 2025 or 2026.
Orienspace’s Gravity-2 is a kerosene-liquid oxygen launcher with a quoted 25,600 kg to LEO and a first flight planned in 2025 with plans for a reusable first stage.
Gravity-2 will use nine 100-ton-thrust Yuanli-85 gas-generator kerosene engines for the first stage.
Earlier payload specifications for Gravity-2 listed capacity as 15,500 kg to LEO, 10,900 kg to a 500-kilometer SSO, and 5,800 kg to GTO.
More recent projected payload capabilities for Gravity-2 are 25,600 kg to LEO, 19,100 kg to SSO, and 7,700 kg to GTO.
Gravity-2 will use a liquid core stage with solid boosters and will provide a payload capacity of 15,500 kg to LEO, 10,900 kg to a 500-kilometer sun-synchronous orbit, or 5,800 kg to geostationary transfer orbit.