SAP100a
YIM
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QUICKLY MODULAR SOLAR PANELS | YIM SAP100a
Microsatellite
Cube satellites are representative of microsatellites and nanosatellites. The initial definition of a cube satellite was an external dimension of 10cm × 10cm × 10cm cube is also known as a cube satellite, consisting of multiple standard cube units (Units), such as 2U cube satellites, 3U cube satellites, 6U cube satellites, etc.
CubeSat Concept Definition
The interface between the solar panel and the satellite varies depending on the manufacturer, provided that the overall dimensions of the cube satellite comply with the specifications of the cube satellite. This product is compatible with ISIS (Innovative Solutions In Space) cubic satellite interfaces (Clyde and other standards can be customized).
Features
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.
Application
1) solar panel (top / bottom)
SAP100 products for the 1U cubic star solar pael top / floor. Optional accessories: solar sensors, temperature sensors, magnetic torque, MEMS gyroscope.
(A) 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.
Used for space solar system projects and space solar power systems, space grade solar cells, and excellent space engineers solar panels.

Specification
SAP100a type 1U cube satellite top / floor
Model | SAP100a | ||
Configuration form | 2S1P | ||
Size (mm) | 98mm×98mm | ||
BOL | Voc(V) | 25℃ | 5.35 |
Vmp(V) | 85℃ | 3.96 | |
Pmp(W) | 25℃ | 2.35 | |
Pmp(W) | 85℃ | 2.04 | |
EOL | Voc(V) | 25℃ | 5.13 |
Vmp(V) | 85℃ | 3.80 | |
Pmp(W) | 25℃ | 2.06 | |
Pmp(W) | 85℃ | 1.86 | |
Summarize: