Space Solar Panel
Guaranteed Life Cycle Voltage / Power BOL / EOL
Material
EM: FR4 PCB, Aluminium PCB
QM: Aluminium honeycomb wings, HDRM, SADA
FM: Carbon Honeycomb (2.6 kg/m2) or Carbon Honeycomb (1.8 kg/m2), HDRM, SADA
We deliver bespoke design for missions depending on mass budget, radiation, power requirements and mission timescale. Get in touch with Sales team, fill in options sheet and we find perfect match to your power requirements. Input from client:
- Voltage and Power, Beginning of Life, End of Life
- Mass budget
- Dimension Budgets
- Fixed / Deployable
- Test requirements (TVAC, Vibration, Burn-In, EMC)
- Quantity of EM, QM, FM
- .Stp file from Satellite structure
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.
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.
Solar Panel Specification
| Model | SAP100a | ||
|---|---|---|---|
| Configuration form | 2S1P | ||
| Size (mm) | 98mm×98mm | ||
| BOL | Voc（V） | 25℃ | 5.35 |
| BOL | Vmp（V） | 85℃ | 3.96 |
| BOL | Pmp（W） | 25℃ | 2.35 |
| BOL | Pmp（W） | 85℃ | 2.04 |
| EOL | Voc（V） | 25℃ | 5.13 |
| EOL | Vmp（V） | 85℃ | 3.80 |
| EOL | Pmp（W） | 25℃ | 2.06 |
| EOL | Pmp（W） | 85℃ | 1.86 |
Solar Panel Specification
| Model | SAP100a | ||
|---|---|---|---|
| Configuration form | 2S1P | ||
| Size (mm) | 98mm×98mm | ||
| BOL | Voc（V） | 25℃ | 5.35 |
| BOL | Vmp（V） | 85℃ | 3.96 |
| BOL | Pmp（W） | 25℃ | 2.35 |
| BOL | Pmp（W） | 85℃ | 2.04 |
| EOL | Voc（V） | 25℃ | 5.13 |
| EOL | Vmp（V） | 85℃ | 3.80 |
| EOL | Pmp（W） | 25℃ | 2.06 |
| EOL | Pmp（W） | 85℃ | 1.86 |
Solar Panels, Guaranteed life cycle Voltage/Power
Modular solar panels (RAMS, 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.
Quickly Modular Solar Panels
Rapidly modular solar panels (RAMS, Rapid Assembling Modular Solar-panle) 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.
solar module RAMS-AP6
6 unit frame RAMS-S6
solar module RAMS-AP4
4 unit frame RAMS-S4
Solar battery module RAMS-M19
SAP100a type 1U cube satellite top - floor
solar module RAMS-AP6
6 unit frame RAMS-S6
solar module RAMS-AP4
4 unit frame RAMS-S4
Solar battery module RAMS-M19
SAP100a type 1U cube satellite top - floor
Solar Panel Specification
| Configuration form | 19S1P | ||
|---|---|---|---|
| Battery size（mm） | 40mm×80mm | ||
| Output voltage（V） | 34V（bus voltage 28~30V） | ||
| Module | power（W） | 22W（25℃，MPPT）~15W（80℃，29V） | |
| Module | Size（mm） | 224mm×330mm（area 729.38cm2） | |
| Module | Weight（kg） | 0.062kg（with circuit 0.1448kg） | |
| Module | Area Specific power （W/m2） | 297.5W/m2（25℃，MPPT）~205.65 W/m2（80℃，29V） | |
| Module | Surface density （kg/m2） | 0.85kg/m2（with circuit 1.98kg/m2） | |
| Module | Mass ratio power （W/kg） | 149W/kg~102.2W/kg | |
| Plate | 4 unit（RAMS-AP4） | 6 unit（RAMS-AP6） | |
| Plate | Power（W） | 88W（25℃MPPT）~60W（80℃，29V） | 132W（25℃MPPT）~90W（80℃，29V） |
| Plate | Size（mm） | 448mm×662mm | 672mm×662mm |
| Plate | Weight（kg） | 0.59kg（with circuit 0.93kg） | 0.89kg（with circuit 1.4kg） |
| Plate | Area Specific power （W/m2） | 296.7 W/m2（25℃，MPPT）~202.3 W/m2（80℃，29V） | |
| Plate | Surface density （kg/m2） | 1.99kg/m2（with circuit 3.1kg/m2） | |
| Plate | Mass specific power （W/kg） | 94.9W/kg（25℃，MPPT）~64.5W/kg（80℃，29V） | |
| Cycle | delivery cycle T0 + 3month, supply capacity 20FM / month |
Solar Panel Specification
| Configuration form | 19S1P | ||
|---|---|---|---|
| Battery size（mm） | 40mm×80mm | ||
| Output voltage（V） | 34V（bus voltage 28~30V） | ||
| Module | power（W） | 22W（25℃，MPPT）~15W（80℃，29V） | |
| Module | Size（mm） | 224mm×330mm（area 729.38cm2） | |
| Module | Weight（kg） | 0.062kg（with circuit 0.1448kg） | |
| Module | Area Specific power （W/m2） | 297.5W/m2（25℃，MPPT）~205.65 W/m2（80℃，29V） | |
| Module | Surface density （kg/m2） | 0.85kg/m2（with circuit 1.98kg/m2） | |
| Module | Mass ratio power （W/kg） | 149W/kg~102.2W/kg | |
| Plate | 4 unit（RAMS-AP4） | 6 unit（RAMS-AP6） | |
| Plate | Power（W） | 88W（25℃MPPT）~60W（80℃，29V） | 132W（25℃MPPT）~90W（80℃，29V） |
| Plate | Size（mm） | 448mm×662mm | 672mm×662mm |
| Plate | Weight（kg） | 0.59kg（with circuit 0.93kg） | 0.89kg（with circuit 1.4kg） |
| Plate | Area Specific power （W/m2） | 296.7 W/m2（25℃，MPPT）~202.3 W/m2（80℃，29V） | |
| Plate | Surface density （kg/m2） | 1.99kg/m2（with circuit 3.1kg/m2） | |
| Plate | Mass specific power （W/kg） | 94.9W/kg（25℃，MPPT）~64.5W/kg（80℃，29V） | |
| Cycle | delivery cycle T0 + 3month, supply capacity 20FM / month |
