Space Solar Panel

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Rapidly modular solar panels (RAMS, Rapid Assembling Modular Solar-panel) with a thin carbon fiber–aluminum honeycomb board as a module structure, combined with carbon fiber–aluminum honeycomb frame structure, through a number of modules and frame assembly, you can achieve solar panels Of the rapid assembly and integration, both as a spacecraft solar array plate can also be used as a development board, the output power range of 15W ~ 530W. Modular solar panels can accommodate existing deployments and drive mechanisms with a total thickness of up to 23 mm.

TECHNICAL SPECIFICATIONS

• Power Range: 2-960 W
• Applications for LEO, GEO & Exploration
• Guaranteed Mission Life Cycle Voltage/ Power
• Re-Insured by Aerospace Insurance Packages
• Highly scalable to mission requirements
• 1-3 panels per wing
• Operating Temperature: -90~+110
• CFRP skin with aluminium honeycomb panel
• Cells: Triple-junction GaAs, 40mm×80mm, E.: 30% or 32%
• Mass: Mechanisms 0,5Kg for a wing of 3 panels , Panel + PVA: 3,4Kg/m2
• Loads: Above15g quasi static design load, Above 15grms random vibration

MATERIAL

• Printed circuit board (PCB): Includes FR4 and multilayer ceramic plates.
  Aluminum-reinforced printed circuit board: Form PCB-Al-PCB, aluminum thickness by default 0.8mm;
• Kapton Aluminum: Aerospace Class Kapton, 6061 Aluminum.
• Thickness specification:
  – 1.6mm;
  – 2.1mm;
  – custom made.
• Solar panel (top / bottom): SAP100 products for the 1U cubic star solar panel top / floor.
• Optional accessories: solar sensors, temperature sensors, magnetic torque, MEMS gyroscope.
• SAP100a type: SAP100a-type selection of products of solar cells, the use of aerospace products
  production process, high reliability, life of not less than 2 years.