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) |
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.
Galactic Energy’s Pallas-1 is a kerosene-liquid oxygen reusable launcher with a payload capacity of 5,000 kg to LEO or 3,000 kg to a 700 km SSO.
Galactic Energy’s Pallas-1 is a kerosene-liquid oxygen reusable launcher with a payload capacity of 5,000 kg to LEO or 3,000 kg to a 700 km sun-synchronous orbit.
Galactic Energy and CAS Space have both conducted VTVL tests using jet-powered prototypes for their Pallas-1 and Kinetica-2 launchers, respectively.
The 1.1 billion yuan funding will support research and development of reusable launch vehicle technology for the Pallas-1 medium-lift rocket and related infrastructure.
Galactic Energy secured $154,000,000 in funding for development of its reusable Pallas-1 rocket.
Galactic Energy plans to launch the triple-core Pallas-1 variant as soon as 2026.
Pallas-1 has a planned payload capacity of 3,000 kg to a 700 km sun-synchronous orbit (SSO).
The triple-core Pallas-1 variant will be capable of lifting 14,000 kg to LEO.
Pallas-1 has a planned payload capacity of 5,000 kg to low Earth orbit (LEO).
Galactic Energy plans recovery of a Pallas-1 first stage using landing legs in 2025.
Pallas-1 has a planned capacity of 3,000 kg to a 700 km sun-synchronous orbit (SSO).
Galactic Energy plans a rocket-powered hop test with Firebird-6 in 2024 as part of Pallas-1 reusable launcher development.
Galactic Energy is planning a triple-core variant of the Pallas-1 capable of lifting 14,000 kg to LEO and planned to launch as soon as 2026.
Pallas-1 is a 42-meter-long kerosene-liquid oxygen (kerolox) launcher with a planned capacity of 5,000 kg to low Earth orbit (LEO).
Galactic Energy plans a first expendable flight of Pallas-1 in the third quarter of 2024.
Galactic Energy performed a hop test with a jet engine-powered test article in August 2023 as part of development of the Pallas-1 kerosene-liquid oxygen reusable launcher.
Galactic Energy performed a hop test with a jet engine-powered article as part of development for the Pallas-1 kerolox reusable launcher.
Pallas-1 is a reusable two-stage launcher capable of carrying 5,000 kg to LEO or 3,000 kg to a 700-kilometer SSO.
Galactic Energy plans a first Pallas-1 flight including recovery of the first stage using landing legs in 2025.