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30% Efficiency 1U solar panel (top/bottom)

QUICKLY MODULAR SOLAR PANELS

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).

Model:
SAP100a
Brand:
YIM

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Product Description

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 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.

SAP100a type 1U cube satellite top / floor

Model		SAP100a
Configuration form		2S1P
Size (mm)		98mm×98mm
BOL	V_oc（V）	25℃	5.35
	V_mp（V）	85℃	3.96
	P_mp（W）	25℃	2.35
	P_mp（W）	85℃	2.04
EOL	V_oc（V）	25℃	5.13
	V_mp（V）	85℃	3.80
	P_mp（W）	25℃	2.06
	P_mp（W）	85℃	1.86

Summarize:

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.