朱雀三号
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 |
|---|---|---|
| 2025 | 1 | 0 |
| 2026 | 0 | 2 |
| 2027 | 0 | 4 |
| 2028 | 0 | 6 |
| 2029 | 0 | 8 |
| 2030 | 0 | 10 |
| 2031 | 0 | 10 |
| 2032 | 0 | 10 |
| 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 | 1 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Zhuque-3 | LEO | 21,000 kg | Unknown | Unknown | SpaceNews Zhuque-3 test flight report |
Zhuque-3 | LEO | 13,000 kg | 200 km | Unknown | chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Zhuque-3 | LEO | 11,100 kg | 450 km |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Dummy payload | Zhuque-3 | Dec 3, 2025 |
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 |
|---|---|---|---|
Zhuque-3 | Not stated | 1 | Active |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Jiuquan Satellite Launch Center | 2 | 35% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2027 | Jiuquan Satellite Launch Center | 4 | 35% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2028 | Jiuquan Satellite Launch Center | 6 | 40% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2029 | Jiuquan Satellite Launch Center | 8 | 40% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2030 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2031 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2032 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2033 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2034 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2035 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2036 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2037 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2038 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2039 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2040 | Jiuquan Satellite Launch Center | 10 | 45% | Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low. |
| 2041 | Jiuquan Satellite Launch Center | 1 | 25% | Catalog-completeness placeholder for active Zhuque-3 family; not used by latest forecast capacity snapshot. |
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
| Unknown |
| chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Zhuque-3 | LEO | 9,400 kg | Unknown | Unknown | chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Zhuque-3 | SSO | 5,400 kg | 800 km | Unknown | chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
Manual 2026-06-06 review: Zhuque-3 is a reusable medium-lift family with published 2026 recovery/production plans; one launch per year is too low.
ESA and the EU SST network forecast the ZhuQue-3 upper stage’s reentry around midday after a final overflight of Germany at about 10:00 local time.
LandSpace’s ZhuQue-3 (ZQ-3) heavy rocket had a second stage that was tracked shortly before reentry.
ZhuQue-3 delivers over 750 tons of liftoff thrust.
Fraunhofer FHR used its space-surveillance radar TIRA to capture a radar image of the ZhuQue-3 upper stage.
ZhuQue-3 has a liftoff mass over 570 tons.
ZhuQue-3 has an overall length of 66.1 meters.
ZhuQue-3 is a large, reusable liquid-fueled launch vehicle independently developed by LandSpace for large-scale constellation deployment missions.
ZhuQue-3 was officially initiated in August 2023.
LandSpace’s Zhuque-3 launch vehicle flew for the first time on December 3rd, 2025.
When flown, the Long March 12B will become China’s third reusable launch solution following LandSpace’s Zhuque-3 and the Shanghai Academy of Spaceflight Technology’s Long March 12A in December 2025.
The startup aims to recover the first stage of the Zhuque-3 rocket by the summer of next year.
Dong Kai, Zhuque-3's Deputy Chief Engineer, stated that a successfully landing first-stage booster will be refurbished for use on the fourth mission.
The full capability version of Zhuque-3 will be able to carry 21,300 kilograms when expended or 18,300 kilograms with first-stage reuse, using TQ-12B engines generating 100 tons of thrust each.
The second Zhuque-3 flight vehicle has completed assembly and is undergoing necessary changes for a first-stage booster landing.
Zhuque-3's first-stage booster test article, fired up in June 2025, could be converted into a flight vehicle.
Zhuque-3's next flight is expected to take place in April 2026.
Zhuque-3's 'full capability' version, standing 76.6 meters tall, is expected to be completed in 2026 for possible flight in 2027.
Zhuque-3 aims to become a low-cost, high-capacity, regularly flying, partially reusable launch vehicle.
In its current design, Zhuque-3 stands 66 meters tall and carries up to 11,800 kilograms of payload using TQ-12A engines generating 83 tons of thrust.
Zhuque-3 had its first flight in June 2025 and focuses on deploying space-based connectivity mega-constellations.