PALLAS-1
Medium Reusable Liquid Launch Vehicle
Pallas-1 is a two-stage liquid launch vehicle with an advanced upper stage, independently developed by Galactic Energy.
It has a body diameter of 3.35 m, a fairing diameter of 4.2 m, a lift-off mass of 283 t, and a lift-off thrust of 350 t-force (3433.5 kN).
It can be optionally equipped with an Eros upper stage, with a maximum payload capacity of 7 t to low Earth orbit.
The first stage of the rocket is capable of vertical recovery, with a designed reuse count of 25 times.
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Configuration
Two-stage / Two-stage + Eros upper stage
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Fairing Diameter
4.2m
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Lift-off Mass
283t
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Payload Capacity
7t@LEO
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·Overall Design Technology of Seven-Engine Parallel Power Redundanc
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·Integrated Structure-Function Design Technology
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·Deep Throttle & Reusable LOX/Kerosene Engine Technology
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·High-Precision Vertical Recovery Guidance & Control Technology for Stage Weak Maneuver
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·Low-Cost Redundant Design of Integrated Control / Measurement / Safety System
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·Reusable Launch Vehicle Health Management Technology
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·Adopts Three-Horizontal & One-Vertical Rapid Test & Launch Mode
