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...
Orien Space plans to conduct Gravity-2's maiden flight within 2026.
Orien Space is shipping rocket engines to Haiyang Space Port for the Gravity-2 launch vehicle.
OrienSpace has been testing YF-102 engines for use on an early version of its Gravity-2 launch vehicle.
Orienspace plans to introduce the Gravity 2 launch vehicle in the near term.
Orien Space plans to have the maiden flight of the Gravity-2 rocket in 2025.
Gravity-2's engine has fired, and the rocket is reported to be ready in 25 days.
Gravity-2 consists of a liquid-fuel core stage and solid rocket boosters, capable of deploying approximately 25.6 tons to LEO.
Gravity-3 uses three core stages of Gravity-2 and can carry five tons more payload than Gravity-2.
Orienspace is developing two additional rockets, Gravity-2 (Yinli-2: YL-2) and Gravity-3 (Yinli-3: YL-3), which are larger and more powerful.
Nine Yuanli-110 engines will power the first-stage of Orienspace’s Gravity-2 rocket.
Orienspace's co-founder claimed that the Gravity-2 could launch this year.
The last test of a Yuanli-110 engine occurred in December 2024 before Orienspace switched to using the YF-102 for its Gravity-2 initial flights.
Orienspace last tested a Yuanli-110 engine in December 2024 before switching to the YF-102 engine for initial Gravity-2 flights.
Orienspace’s Gravity-2 uses kerolox propellant, has a payload capacity of 25,600 kg to LEO, has a first flight planned in 2025, and plans a reusable first stage.
Orienspace’s Gravity-2 is a kerolox rocket with 25,600 kg to LEO capability, a first flight in 2025, and plans for a reusable first stage.
Orienspace is developing the Gravity-2 kerolox launcher with a payload capacity of 25,600 kg to low Earth orbit, a planned first flight in 2025, and plans for a reusable first stage.
Orienspace’s Gravity-2 has a stated payload capacity of 25,600 kg to low Earth orbit with first flight planned in 2025 and plans for a reusable first stage.
Orienspace’s Gravity-2 is a kerolox rocket with a payload capacity of 25,600 kg to low Earth orbit and a first flight planned in 2025 with plans for a reusable first stage.
Orienspace is developing the Gravity-2 kerolox rocket with a payload capacity of 25,600 kg to LEO and a first flight planned in 2025.
Gravity-2 is a 60-meter-tall, 4.2-meter-diameter rocket developed by Orienspace.