English 
SAP100a
YIM
| Quantity: | |
|---|---|
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.
1) 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.
(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.
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 | |
The classification and definition of satellites are different. Generally speaking, satellites weighing less than 1000kg are called microsatellites, and those weighing less than 100kg are called microsatellites (MicroSat). Some people also call 10~150kg satellites microsatellites, and 100~500kg satellites are generally called MiniSats abroad. Therefore, in this paper, 10~500kg satellites are collectively called microsatellites. Compared with traditional Star of David, microsatellites are characterized by low cost, short cycle, high flexibility, reconfiguration and rapid response, and have broad prospects in military, commercial remote sensing, commercial meteorology, satellite Internet, technical verification, scientific exploration and other fields. We have launched a fast modular solar panel product tailored to the characteristics of microsatellites.
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.
1) 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.
(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.
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 | |
The classification and definition of satellites are different. Generally speaking, satellites weighing less than 1000kg are called microsatellites, and those weighing less than 100kg are called microsatellites (MicroSat). Some people also call 10~150kg satellites microsatellites, and 100~500kg satellites are generally called MiniSats abroad. Therefore, in this paper, 10~500kg satellites are collectively called microsatellites. Compared with traditional Star of David, microsatellites are characterized by low cost, short cycle, high flexibility, reconfiguration and rapid response, and have broad prospects in military, commercial remote sensing, commercial meteorology, satellite Internet, technical verification, scientific exploration and other fields. We have launched a fast modular solar panel product tailored to the characteristics of microsatellites.
