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 completed a static fire test of Pallas-1's second stage.
Galactic Energy has static fired the second stage of the Pallas-1.
A successful second stage static fire test was conducted for Pallas-1.
Galactic Energy is preparing for the debut flight of the kerolox Pallas-1 rocket.
The first Pallas-1 is expected to arrive at the Jiuquan Satellite Launch Center in November 2023 for its debut flight.
Galactic Energy is preparing to debut its partially reusable Pallas-1 and larger solid-fueled Ceres-2 launch vehicles.
The Pallas-1 rocket is expected to weigh around 283,000 kilograms at launch and can carry a payload of up to 8,000 kilograms.
Pallas-1's S2 is equipped with SL Welkin and a crude nozzle extension.
Pallas-1 will have a payload capacity of 8,000 kg to a 200-kilometer low Earth orbit and a future three-core variant will be capable of carrying up to 30,000 kg to LEO.
Galactic Energy plans to launch Pallas-1 from new facilities at the Hainan commercial spaceport and is constructing a dedicated site at the Dongfeng Commercial Space Innovation Test Area at Jiuquan Satellite Launch Center.
Pallas-1 is planned to be adapted for first-stage reusability and to have a payload capacity of 8,000 kg to a 200-kilometer-altitude low Earth orbit.
Galactic Energy is developing the Pallas-1 kerosene-liquid oxygen launch vehicle with a targeted debut flight in 2025.
Galactic Energy’s Pallas-1 uses kerosene-liquid oxygen propellant and has a payload capacity of 5,000 kg to LEO or 3,000 kg to a 700 km sun-synchronous orbit.
Galactic Energy’s Pallas-1 is a kerosene-liquid oxygen rocket with a payload capacity of 5,000 kg to LEO or 3,000 kg to a 700 km sun-synchronous orbit.
Galactic Energy is developing the Pallas-1 kerosene-liquid oxygen launcher with a payload capacity of 5,000 kg to low Earth orbit or 3,000 kg to a 700 km sun-synchronous orbit.
Galactic Energy is working towards the first launch of the Pallas-1 kerosene-liquid oxygen rocket with the first flight expected later in 2024 and likely to be expendable.
Galactic Energy’s Pallas-1 has a stated payload capacity of 5,000 kg to low Earth orbit or 3,000 kg to a 700-kilometer sun-synchronous orbit.
Galactic Energy is developing the Pallas-1 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 is developing the Pallas-1 kerosene-liquid oxygen reusable rocket with a payload capacity of 5,000 kg to LEO or 3,000 kg to a 700-kilometer sun-synchronous orbit.
Galactic Energy plans at least 10 Ceres-1 solid rocket launches in 2024 and plans to debut the kerolox Pallas-1 in 2024.