Pallas-1
Pallas-1
Space Launch Systems
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
Pallas-1
Designation
Pallas-1
Alternate Designation
—
Equipment Type
Space Launch Systems
Manufacturer
—
Date of Introduction
2027
Description
The Pallas-1 is a medium class space launch system with a reusable first stage capable of delivering a 5-ton payload to Low Earth Orbit (LEO). The Pallas-1 launch system was developed by Galactic Energy of China. The first stage is powered by seven Welkin engines burning a mix of kerosene and liquid oxygen (LOx). The first launch of the Pallas-1 space launch system was carried out on September 1, 2026. Pallas-1B is a further development intended to send a payload of 17-ton into LEO by using three Pallas-1 first stages.
Overview (Deagel)
Group
Space Launch Systems
Status
Under Development
Origin
China
Initial Operational Capability (IOC)
2027
First Flight
September 1, 2026
Total Production
1
Specifications (Deagel)
Number of Stages
3
Dimensions — Height
42 meter
Dimensions — Rocket Diameter
3.4 meter
Mass — Max Lift-off Thrust
357 ton
Mass — Max Lift-off Weight
220 ton
Mass — Payload to LEO
5,000 kilogram
Mass — Payload to SSO
3,000 kilogram
Details
Country of Origin
China
Sources
deagel.com: https://www.deagel.com/x/x/a004745
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
—
Height
42 m
Weight
—
Operators (1)
China
Something went wrong. Please reload the page.
Reload