CERES-1
Small-lift Launch Vehicle
The "Ceres-1" launch vehicle is capable of providing cost-effective launch services for various low- and medium-small satellites; it is equipped with multiple satellite installation interfaces and can design multiple interfaces according to user needs, making it convenient for users to select and use.
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Configuration
Three-stage solid + liquid upper stage
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Diameter
1.4m/1.6m
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Lift-off mass
32.7t
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Payload capacity
300kg@SSO、420kg@LEO
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·Integrated Integration Technology for Rocket Upper Stage Structure/Propulsion/Electrical System
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·High-Precision Navigation Technology for Vertical Self-Alignment and On-line Misalignment Angle Correction of Marine Dynamic Base
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·Simplified Control Technology for First-Stage without Roll Control Device
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·Modular Multi-Satellite Separation Timing Design Technology
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·Simple and Safe Fairing Separation Technology for Launch Vehicle Based on Single Spring
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·Rapid and Safe Active Deorbiting Technology for Rocket Upper Stage
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·Parameter Orthogonalization 3D Modal Accurate Prediction Technology
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·Highly Integrated/Low-Cost/Integrated Electrical System Technology
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·Low-Cost Space-Based S-Band High Bit Rate Telemetry Technology
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·Lightweight and Multi-Functional Special-Shaped Composite Upper Stage Integrated Bracket Design and Forming Technology
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·Distributed Pressurized Separation Orbit Attitude Control Propulsion System Technology
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·All-Metal 3D Printed Orbit Control Engine Technology
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·Multi-Functional Miniaturized Orbit Attitude Control Valve Design Technology
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·Low-Cost Unattended Land-Sea Universal Transfer and Launch Vehicle Technology
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·Solid Rocket Non-Pyrotechnic Locking and Release Technology
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·Solid Rocket Marine Unguided Hot Launch Technology
