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) |
GALACTIC-ENERGY has completed the assembly of the Pallas-1 (Y1) flight vehicle.
GALACTIC-ENERGY has completed the assembly of the Pallas-1 (Y1) flight vehicle.
Galactic Energy's Pallas-1 is almost ready for its first flight.
The launch of Pallas LC Pallas-1 Y1 is scheduled for HCSLC in Q4 2026.
Pallas LC Pallas-1 Y1 is planned for launch in HCSLC in Q4 2026.
Galactic Energy shared recent pictures of Pallas LC Pallas-1 Y1, which is expected to be delivered at JSLC at the end of December.
Pallas LC Pallas-1 Y1 is expected to be delivered at JSLC at the end of December.
Pallas-1 will be 42 meters tall and 3.35 meters in diameter when prepared for flight later this year.
Galactic Energy's two-stage partially reusable launch vehicle, Pallas-1, has conducted two critical pre-debut flight tests.
Pallas-1 is planned to carry 8,000 kilograms into low Earth orbit while returning its first-stage to Earth using four grid fins.
A second-stage firing for Pallas-1 was completed in September, followed by a seven-engine first-stage static fire in November.
Galactic Energy's Pallas-1 has completed its first and second-stage static fires.
Pallas-1's main engine CQ-50 was throttled down to 32%.
GALACTIC-ENERGY completed more tests of Pallas-1's main engine CQ-50.
Pallas-1's main engine CQ-50 was throttled up to 105%.
The race to fly a reusable rocket in China's commercial space sector now includes Space Pioneer with Tianlong-3, LandSpace with Zhuque-3, Galactic Energy with Pallas-1, and CAS Space with Kinetica-2.
The 7-engine configuration is possible for the Pallas-1.
Galactic Energy announced on November 4th that Pallas-1's first-stage conducted its static fire, igniting seven CQ-50 engines.
Pallas-1's first-stage static fire was conducted on a floating platform near Haiyang, Shandong province.
Pallas-1 is set to debut from the Jiuquan Satellite Launch Center via a dedicated launch pad currently under construction.