HARDWARE / PRODUCTUpdated 24 Jul 2026

Ra

Spacemanic s.r.o.
Ra

Ra is Spacemanic’s high-efficiency solar panel solution, engineered for nanosatellites and beyond, delivering reliable, mission-optimized energy for any platform size.

Typed specifications109 values

Discloses 10 of 12 fields engineers filter by in this category (category median 3).

Mass
30 g
1U, typical · datasheet p.3 30 g 1U  |  70 g 2U  |  70 g 2U, typical  |  110 g 3U  +9
Output power (BOL)
2.48 W
1U · datasheet p.3 2.48 W 1U panel, BOL peak power @ LEO  |  4.96 W 2U  |  4.96 W 2U panel, BOL peak power @ LEO  |  8.68 W 3U  +9
Cell efficiency
25.7 %
EOL · datasheet p.3 25.7 % EOL (1e15 e/cm2), AM0 25 °C  |  30 % min · BOL  |  30 % min · BOL, > 30 %, AM0 25 °C
Envelope (L×W×H)
1U
Typical · datasheet p.3
Form factor (as printed)
1U
datasheet p.3 2U  |  3U  |  6U body-mounted  |  6U deployable  +2
Deployable
no
6U body-mounted · datasheet p.3 yes 6U deployable  |  yes 6U deployable / 8U deployable configurations (customization o…  |  no 8U body-mounted  |  yes 8U deployable  +1
Supply voltage
0 V
min · datasheet p.4 20 V max
Power consumption
2.48 W
1U @ LEO · datasheet p.3
Operating temperature
-40 °C
min · datasheet p.3 125 °C max  |  -40–125 °C
Array configuration
body-mounted panel
typical configurations; deployable option available · datasheet p.3
Fits satellite size
1U
datasheet p.3 2U  |  3U  |  6U  |  8U
Cell type
triple-junction GaAs
state-of-the-art triple junction solar cells · datasheet p.3
Open-circuit voltage at the panel output (Voc)
2.75 V
BOL @ AM0 (135.3 mW.cm-2) and 25 °C · datasheet p.3 2.48 V EOL (10^15 e.cm-2) @ AM0 (135.3 mW.cm-2) and 25 °C
Max-power voltage at the panel output (Vmp)
2.48 V
BOL @ AM0 (135.3 mW.cm-2) and 25 °C · datasheet p.3 2.26 V EOL (10^15 e.cm-2) @ AM0 (135.3 mW.cm-2) and 25 °C
Number of strings
1
1U, 2S1P · datasheet p.3 1 2U, 4S1P  |  1 3U, 7S1P  |  2 6U body-mounted, 7S2P  |  4 6U deployable, 4S4P  +3
Integrated devices
bypass diodes
optional · datasheet p.3 magnetorquer coil optional panel-mounted magnetorquer  |  other optional patch antennas; mechanical interface for FSS; RBF cu…  |  coarse sun sensor optional, CSS / SLCD sun sensor with MCP3221 ADC  |  temperature sensor optional, TMP112
Connector
MOLEX PicoBlade connector (53261-0471)
datasheet p.4
Flight heritage
10+ missions (e.g. LASARsat, CroCube, GRBBeta and external customers)
datasheet p.3
Satellite class
CubeSat
related 1-16U CubeSat platforms; 1U-8U sizes · datasheet p.3
Missions flown
10
datasheet p.3 10 min · flight heritage on 10+ missions
Max-power current (Imp)
0.5 A
BOL @ AM0 (135.3 mW.cm-2) and 25 °C · datasheet p.3 0.46 A EOL (10^15 e.cm-2) @ AM0 (135.3 mW.cm-2) and 25 °C  |  0.5 A per solar cell, BOL, AM0 (135.3 mW/cm2) 25 °C  |  0.46 A per solar cell, EOL (1e15 e/cm2), AM0 25 °C
Short-circuit current (Isc)
0.52 A
BOL @ AM0 (135.3 mW.cm-2) and 25 °C · datasheet p.3 0.49 A EOL (10^15 e.cm-2) @ AM0 (135.3 mW.cm-2) and 25 °C  |  0.52 A per solar cell, BOL, AM0 (135.3 mW/cm2) 25 °C  |  0.49 A per solar cell, EOL (1e15 e/cm2), AM0 25 °C
Substrate
other
PCB, typical PCB material 370HR · datasheet p.3
Number of cells
2
1U, typical · datasheet p.3 4 2U, typical  |  7 3U, typical  |  14 6U body-mounted, typical  |  16 6U deployable, typical  +2
Cells per string
2
1U, 2S1P · datasheet p.3 4 2U, 4S1P  |  7 3U, 7S1P  |  7 6U body-mounted, 7S2P  |  4 6U deployable, 4S4P  +3
Deployment mechanism (as printed)
Body-mounted/deployable
datasheet p.3
Integrated sensors (as printed)
Optional: panel-mounted temperature sensor (TMP112), sun sensor CSS (SLCD, ADC MCP3221), mechanical interface for FSS, magnetorquer
datasheet p.3
Panel thickness
1.6 mm
typical PCB thickness · datasheet p.3
Bypass diodes
other
optional bypass protection diode (0,8 V @ 620 mA) · datasheet p.3

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier17 lines, in the manufacturer's own wording
Flight heritage
Yes
ITAR free
Yes
Operating temperature
-40°C to +125°C
Efficiency
> 30%
Configurations
1U, 2U, 3U, 6U, 8U + customized design
Typical power harvest
up to 1.2 W per cell: 1U (2 cells) 2.4 W, 2U (4 cells) 4.8 W, 3U (7 cells) 8.4 W, 6U (16 cells) 19.2 W, 8U (20 cells) 24.0 W
Mass
30 g (typical 1U)
Mass (typical)
230 g (typical 6U)
Customization options
Body-mounted
Customization options (2)
Deployable
Customization options (3)
Structural panel (no cells)
Customization options (4)
Cutouts
Customization options (5)
Temperature sensors, Sun-sensors
Customization options (6)
Magnetorquer
Customization options (7)
Patch antennas
Customization options (8)
Bypass protection diode
Customization options (9)
Mechanical and electrical interface

About

Ra is a high-efficiency solar panel solution developed by Spacemanic, designed for nanosatellites and other space platforms. It is built with premium solar cells and can be tailored to match a satellite’s structure and power profile, ensuring reliable and mission-optimized energy. The product is ITAR free and offers a wide range of customization options due to in-house developed hardware and software. Customization includes body-mounted or deployable configurations, structural panels without cells, cutouts, and integration of temperature sensors, sun-sensors, magnetorquers, patch antennas, bypass protection diodes, and specific mechanical and electrical interfaces. Each panel is designed to fit the satellite’s specifications, including custom features and cutouts. The product includes custom panels, a CAD model, one hour of engineering support, and shipping and packaging. Lead time ranges from 3 to 7 months, depending on solar cell availability. Ra offers high efficiency, with typical power harvest up to 1.2 W per cell, and configurations for 1U, 2U, 3U, 6U, and 8U satellites, as well as customized designs. It has flight heritage.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: spacemanic.com ↗

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