朱雀二号
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 |
|---|---|---|
| 2022 | 1 | 0 |
| 2023 | 2 | 0 |
| 2024 | 1 | 0 |
| 2025 | 2 | 0 |
| 2026 | 2 | 1 |
| 2027 | 0 | 1 |
| 2028 | 0 | 1 |
| 2029 | 0 | 1 |
| 2030 | 0 | 1 |
| 2031 | 0 | 1 |
| 2032 | 0 | 1 |
| 2033 | 0 | 1 |
| 2034 | 0 | 1 |
| 2035 | 0 | 1 |
| 2036 | 0 | 1 |
| 2037 | 0 | 1 |
| 2038 | 0 | 1 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Zhuque-2 | LEO | 6,000 kg | 200 km | Unknown | Gunter Krebs / Skyrocket Zhuque-2 profile |
Zhuque-2E | LEO | 6,000 kg | 200 km | Unknown | LandSpace products page |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Qianfan DTC1/ZYD-02 | Zhuque-2E | Jun 9, 2026 |
| Dummy sat | Zhuque-2E | May 14, 2026 |
| Launch 2025-F07 | Zhuque-2E | Aug 15, 2025 |
| Tianyi |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Zhuque-2 | Not stated | 3 | Active |
Zhuque-2E | Not stated | 5 | Active |
| 2039 | 0 | 1 |
| 2040 | 0 | 1 |
| 2041 | 0 | 1 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2027 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2028 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2029 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2030 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2031 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2032 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2033 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2034 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2035 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2036 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2037 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2038 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2039 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2040 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
| 2041 | Dongfeng Commercial Space Innovation Test Zone | 1 | 30% | Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot. |
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Zhuque-2E |
| SSO |
| 4,000 kg |
| 500 km |
| Unknown |
| LandSpace Zhuque-2E launch report |
Zhuque-2 | SSO | 1,500 kg | 500 km | Unknown | Xinhua Zhuque-2 profile |
Zhuque-2E |
| May 17, 2025 |
| Guangchuan-01/02 | Zhuque-2E | Nov 27, 2024 |
| Hongqing-1/2/TY-33 | Zhuque-2 | Dec 8, 2023 |
| Dummy payload | Zhuque-2 | Jul 12, 2023 |
| Launch 2022-F05 | Zhuque-2 | Dec 14, 2022 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Catalog-completeness placeholder for active Zhuque-2 family; not used by latest forecast capacity snapshot.
Four TQ-12 engines will power the first stage of the 48.8-meter-tall, 3.35-meter-diameter Zhuque-2 launcher.
The Zhuque-2 launcher is to be capable of delivering a 4,000-kilogram payload to a 200-kilometer low Earth orbit.
The Zhuque-2 will be capable of delivering a 2,000-kilogram payload to a 500-kilometer Sun-synchronous orbit.
LandSpace reached agreements with UK-based Open Cosmos and Italy-based D-Orbit related to launch services involving the Zhuque-2 rocket.
The Zhuque-2 will be capable of delivering a 4,000-kilogram payload to a 200-kilometer low Earth orbit.
LandSpace expects the Zhuque-2 to be the first Chinese rocket powered by methalox propellant and to conduct a test flight expected in 2020 with the third-highest thrust level among commercial aerospace companies globally.
LandSpace has completed assembly of an 80-ton thrust Tianque-12 (TQ-12) liquid methane-liquid oxygen rocket engine for the Zhuque-2 launch vehicle.
LandSpace will use the TQ-12 engine for its Zhuque-2 (Vermillion Bird-2) medium-lift launch vehicle.
Landspace intends Zhuque-2 to be the first Chinese rocket powered by methalox propellant and expects its test flight in 2020.
The TQ-12 engine will power the medium-lift Zhuque-2 launch vehicle that measures 48.8 m tall with a diameter of 3.35 m.
Zhuque-2 is designed to deliver 4,000 kg to a 200-kilometer low Earth orbit and 2,000 kg to a 500-kilometer sun-synchronous orbit.
Landspace is developing a liquid methane-liquid oxygen launcher named Zhuque-2 (Vermillion Bird-2) at a site in Huzhou, Zhejiang province.
Zhuque-2 will be capable of delivering 4,000 kg to a 200-kilometer low Earth orbit and 2,000 kg to a 500-kilometer sun-synchronous orbit using 80-ton and 10-ton methane engines.
Landspace tested gas generators and combustion chambers for the Tianque-12 80-ton-thrust liquid methane/liquid oxygen engine intended to power the two-stage Zhuque-2.
The two-stage Zhuque-2 (ZQ-2) is planned to be 48.8 m tall with a diameter of 3.35 m and to debut in 2020 with an initial manufacturing target of next year.
Zhuque-2 is designed to deliver 4,000 kg to a 200-kilometer low Earth orbit and 2,000 kg to a 500-kilometer sun-synchronous orbit using 80-ton and 10-ton methalox engines.
Landspace planned larger three-stage Zhuque-2 series rockets with variable-thrust engines intended to enable vertical landings and reuse of first stages and to carry up to 32,000 kg to 200-kilometer low Earth orbit.
Zhuque-2 will be capable of delivering 4,000 kg to a 200-kilometer low Earth orbit and 2,000 kg to a 500-kilometer Sun-synchronous orbit using 80-ton and 10-ton methane engines.
The Tianque engine was developed from scratch and will power the larger medium-lift Zhuque-2 launch vehicle.
Zhuque-2 is a Chinese rocket that Landspace envisions launching in 2020 and that also burns methane.