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.
Landspace executed a 350-meter VTVL test using the Zhuque-3 VTVL-1 test article in January 2024.
The 2024-09-11 Zhuque-3 VTVL-1 test included a four-piece grid fin system.
The Zhuque-3 reusable launcher is constructed from stainless steel and uses methane-liquid oxygen (methalox) propellant.
Landspace’s Zhuque-3 is a methalox rocket with up to 21,000 kg payload capacity to LEO and a first flight planned for 2025.
Landspace is developing the methane-liquid oxygen Zhuque-2 and the planned stainless-steel Zhuque-3 launchers.
Landspace’s Zhuque-3 is a methalox launcher with a payload capacity up to 21,000 kg to low Earth orbit and a first flight planned for 2025.
Zhuque-3 is designed with a 4.5-meter diameter and a payload capability of 21,000 kg to low Earth orbit when flown expendably.
Landspace’s Zhuque-3 has a stated payload capacity up to 21,000 kg to low Earth orbit and a first flight planned for 2025.
Landspace is developing the Zhuque-3 stainless steel methane-liquid oxygen reusable rocket at Jiuquan.
Landspace is developing the methane-liquid oxygen Zhuque-2 and a planned stainless steel Zhuque-3 reusable launchers.
Landspace’s Zhuque-3 is a methalox reusable rocket with a payload capacity up to 21,000 kg to low Earth orbit and its first flight is planned for 2025.
Landspace is developing the Zhuque-3 methalox reusable rocket with a payload capacity up to 21,000 kg to LEO and a first flight planned for 2025.
Landspace aims to launch three Zhuque-2 methalox rockets in 2024 and to conduct further hop tests for the stainless steel Zhuque-3.
Multiple Chinese companies are developing reusable rockets, including iSpace’s Hyperbola-3, Landspace’s Zhuque-3, Galactic Energy’s Pallas-1, CAS Space’s Kinetica 2, Deep Blue Aerospace’s Nebula-1, and Space Pioneer’s Tianlong-3.
Landspace’s Zhuque-3 is a methalox reusable launcher with a payload capacity up to 21,000 kg to LEO and a first flight planned for 2025.
The Zhuque-3 VTVL-1 test article reached an altitude of around 350 m during a roughly 60-second flight.
Landspace executed a first vertical takeoff, vertical landing (VTVL) test with the Zhuque-3 VTVL-1 test article at a launch and recovery site at Jiuquan Satellite Launch Center on 2024-01-19 at 0800 UTC (3:00 a.m. Eastern).
Zhuque-3 will have a liftoff mass of about 660,000 kg and will be powered by nine Tianque-12B engines.
Zhuque-3 will carry up to 12,500 kg to LEO when the first stage returns to the launch site.
Zhuque-3 will carry up to 18,300 kg to LEO when the first stage is recovered downrange.