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 is a reusable two-stage launcher that will be capable of carrying 5,000 kg to LEO or 3,000 kg to a 700-kilometer sun-synchronous orbit.
Galactic Energy plans a first Pallas-1 flight including recovery of the first stage using landing legs in 2025.
Pallas-1 will be capable of carrying 5,000 kg to low Earth orbit or 3,000 kg to a 700-kilometer sun-synchronous orbit.
Galactic Energy plans a triple-core variant of Pallas-1 as soon as 2026 that will be capable of lifting 14,000 kg to low Earth orbit.
Galactic Energy plans a test launch of Pallas-1 in 2024 with a payload capacity of 5,000 kg to LEO or 3,000 kg to 700-kilometer SSO.
Galactic Energy’s Pallas-1 reusable kerosene-liquid oxygen launcher has a payload capacity of 5,000 kg to LEO and 3,000 kg to a 700-kilometer SSO and will have its test launch in 2024.
Galactic Energy is developing the Pallas-1 reusable kerosene-liquid oxygen launcher to deliver 5,000 kg to low Earth orbit or 3,000 kg to 700-kilometer sun-synchronous orbit.
Galactic Energy expected a Pallas-1 test launch as early as the first half of 2023 but plans to continue development through 2023.
Galactic Energy is developing a two-stage kerosene-LOX launcher called Pallas-1 designed to carry 5,000 kg to LEO or 3,000 kg to a 700-kilometer SSO.
Galactic Energy’s Pallas-1 and iSpace’s Hyperbola-2 could launch in 2023.
Galactic Energy is developing the two-stage kerosene-liquid oxygen Pallas-1 designed to carry 5,000 kg to LEO or 3,000 kg to a 700-kilometer SSO.
Pallas-1 is a reusable kerosene-liquid oxygen launcher being developed by Galactic Energy.
Pallas-1 is planned to be capable of lofting 5,000 kg to low Earth orbit or 3,000 kg to 700-kilometer Sun-synchronous orbit.
Galactic Energy secured $200,000,000 in funding for Pallas-1 in January, which was the largest funding round of any launch company in China at that time.
Pallas-1 could launch as soon as the first half of 2023.
Galactic Energy plans a first launch of the Pallas-1 launcher in 2023.
Galactic Energy secured $200,000,000 in January and will use the funds for upcoming launches of the Ceres-1 solid rocket and the larger kerosene-LOX Pallas-1 launcher.
Galactic Energy reached orbit twice with its Ceres-1 solid rocket and is developing the VTVL-capable Pallas-1 liquid rocket targeting launch around early 2023.
Pallas-1 is designed to carry 3,000 kg to a 700-kilometer Sun-synchronous orbit.
Pallas-1 is a two-stage medium-lift reusable launch vehicle designed to carry 5,000 kg to low Earth orbit.