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 second stage of ZQ 3 Y1 uses a single TQ-15A engine.
Landspace attempted to vertically land the first stage of the Zhuque-3 methane-liquid oxygen rocket, which ended in a catastrophic failure.
The ZQ 3 Y1 rocket produces more than 750 tons of thrust at liftoff.
The first stage of ZQ 3 Y1 is equipped with nine TQ-12A engines providing the main ascent thrust.
Sentinel-2 provides images important for monitoring Zhuque-3's landing site.
The Zhuque-3 is part of China's strategy to develop a reusable heavy-lift launch vehicle to compete with SpaceX's Falcon 9.
The test verified the overall launch and flight plan for Zhuque-3 and confirmed the compatibility of interfaces between major systems on the vehicle.
The ZQ 3 Y1 vehicle, built mainly from stainless steel, lifted off at noon from a dedicated launch service tower at the Jiuquan Satellite Launch Center in the Inner Mongolia autonomous region.
A single upper-stage engine carried a mass simulator toward low Earth orbit during the ZQ 3 Y1 mission.
LANDSPACE successfully launched the Zhuque-3 rocket for the first time in December 2025.
LandSpace reported that ZQ 3 Y1 is 66.1 meters tall with a diameter of 4.5 meters and a fully fueled mass of about 570 metric tons.
The liftoff of Zhuque-3 was captured by a DJI MAVIC drone.
The Zhuque-3 has a landing pad designed to endure impact.
The attempt to recover the Zhuque-3 booster via a powered vertical descent ended when the stage exploded upon contact with the landing zone.
LANDSPACE unveiled the Zhuque-3 rocket design in December 2023.
The ZQ 3 Y1 has the capacity to deploy heavy satellites into low Earth orbit and sun-synchronous orbits.
Zhuque-3's 'block one' version can lift 8,000 kilograms to low Earth orbit with a first-stage landing downrange.
Fairing separation for Zhuque-3 will occur at T+05:24.
Zhuque-3 will liftoff at T+00:00.
The first-stage ascent of Zhuque-3 was entirely successful, achieving clean separation of the second-stage.