智神星一号
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 |
|---|---|---|
| 2026 | 0 | 6 |
| 2027 | 0 | 6 |
| 2028 | 0 | 6 |
| 2029 | 0 | 6 |
| 2030 | 0 | 6 |
| 2031 | 0 | 6 |
| 2032 | 0 | 6 |
| 2033 | 0 | 6 |
| 2034 | 0 | 6 |
| 2035 | 0 | 6 |
| 2036 | 0 | 6 |
| 2037 | 0 | 6 |
| 2038 | 0 | 6 |
| 2039 | 0 | 6 |
| 2040 | 0 | 6 |
| 2041 | 0 | 6 |
1 launch location represented.
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Pallas-1 | LEO | 7,000 kg | Unknown | Unknown | Galactic Energy Launch Vehicles |
Pallas-1 | LEO | 7,000 kg | 200 km | Unknown | chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Pallas-1 | SSO | 5,000 kg | 700 km | Unknown |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
No recent missionsNo launched missions are linked to variants in this family. | ||
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 |
|---|---|---|---|
Pallas-1 | Not stated | 0 | Active |
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2027 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2028 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2029 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2030 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2031 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2032 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2033 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2034 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2035 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2036 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2037 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2038 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2039 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2040 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
| 2041 | Jiuquan Satellite Launch Center | 6 | 20% | Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Si... |
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
Chinese commercial development launcher; low-confidence conservative default informed by China high national launch cadence and early commercial maturation. Site mapping: Recent P...
| chinese_launch_vehicle_chart_normalized.xlsx (manual screenshot transcription; extraction date 2026-06-02 UTC) |
Pallas-1 Y1 is planned to make its maiden launch in mid-to-late August 2026.
The Pallas-1 pad at Jiuquan Satellite Launch Center is officially completed.
Pallas-1 Y1 is already at Jiuquan Satellite Launch Center.
Galactic Energy placed its first Pallas-1 launch vehicle on its launch pad at the Jiuquan Satellite Launch Center.
Galactic Energy's Pallas-1 is designed for 25 reuses and about 7 tonnes of low-Earth-orbit payload capacity.
Galactic Energy's Pallas-1 is scheduled to launch on June 19, 2026.
Galactic Energy's Pallas-1 uses a first-flight no-recovery strategy, seven liquid oxygen-kerosene engines, and 350 tonnes of thrust.
Galactic Energy completed more tests of Pallas-1's main engine CQ-50.
Pallas-1's main engine CQ-50 can throttle down to 32% and up to 105%.
Galactic Energy said the initial Pallas-1 flights are not expected to include grid fins or landing legs.
Galactic Energy said the launch pad supporting Pallas-1 at the Jiuquan Satellite Launch Center is complete.
Pallas-1 is a partially reusable launch vehicle developed by Galactic Energy.
Galactic Energy’s Phase One plan at Jiuquan is intended to support the high-frequency, large-scale launch of liquid-propellant rockets and the development and operation of Pallas-1 and subsequent rocket systems.
Pallas-1 will weigh about 283,000 kilograms when loaded with rocket-grade kerosene and liquid oxygen.
Pallas-1’s first-stage static fire used seven CQ-50 engines and included coordinated throttling of thrust levels up to 350 tons and gimbaling.
Pallas-1’s first stage arrived in Haiyang, Shandong province, in November 2025 for a pre-debut flight static fire.
Pallas-1 is one of a handful of reusable launch solutions operational in China.
Galactic Energy said it made progress on reusable Pallas-1 hardware such as grid fins and landing legs.
Pallas-1 has two 3.35-meter-diameter stages.
Pallas-1 will stand about 42 meters tall when ready to fly.