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.
The first and second stages of the Zhuque-3 rocket have a diameter of 4.5 meters, and the fairing has a diameter of 5.2 meters.
The Zhuque-3 rocket can deliver a payload of 18.3 tons to Low Earth Orbit (LEO) if the booster is recovered and 21.3 tons if it is disposed of.
LandSpace Technology launched the Zhuque-3 (LandSpace-3: LS-3, Zhuque-3: ZQ-3) rocket for the first time on December 3.
China's Zhuque-3 rocket test flight this week was its first attempt to replicate U.S. rocket reusability.
The ZhuQue-3 launch occurred on December 5, 2025, at 01:52:24 UTC.
The Zhuque-3 test flight ended in explosive failure.
The booster of the Zhuque-3 rocket is equipped with nine Tianque-12A engines.
The Zhuque-3 rocket consists of a reusable first stage and a disposable second stage.
The Zhuque-3 rocket uses grid fins and a Reaction Control System (RCS) to maintain orientation and steer for landing.
The Zhuque-3 rocket achieved successful orbital insertion before the landing attempt.
Zhuque-3 has a height of about 66 meters, a diameter of 4.5 meters, and a liftoff mass close to 560 - 570 metric tons, designed to place heavy payloads into low Earth and sun-synchronous orbits.
Zhuque-3 is LandSpace's first heavy-lift platform aimed at reflight of the first stage.
The first stage of Zhuque-3 is equipped with grid fins and four deployable landing legs to enable vertical landings on a pad in the downrange recovery zone.
LandSpace has indicated that Zhuque-3 will continue through a stepwise test campaign to refine hardware and software toward operational reusability.
The first stage of the Zhuque-3 performed its duties and successfully delivered its payload into orbit.
Recovery attempts in other reusable programs have also experienced early failures, and analysts describe the ZQ 3 Y1 flight as part of the normal development path for a new booster.
The ZQ 3 Y1 mission lifted off around noon local time with nine methane-fueled engines powering the first stage.
Zhuque-3 is built around stainless-steel propellant tanks and methane engines, balancing structural strength, temperature resistance, corrosion resistance, and production cost while supporting multiple uses of the first stage.
Zhuque-3 successfully lifted off.
Zhuque-3 is a space launch vehicle developed by LandSpace.