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1U Z Solar Panel

Power Efficiency: ≥30%
Max Power: 2.4W
Internal By-pass diode: reverse bias protection
Solar cells thickness: 150μm ± 20μm
Sensors: Temperature and Sun (optional Gyroscope)
Available with integrated magnetorquer
Compatible with EnduroSat UHF Antenna
Max Voltage: 4.8V (for 2 cells)
Max Current: 504mA
PCB Thickness: 1.6mm
Mass: ≤48g (57.5g with magnetorquer)

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Платформа КубСат 1U
Flight-proven fully integrated CubeSat bus with unmatched
payload capacity in the 1U class

Feautures :
Bus Mass - 850 g
Available Payload Mass - 500 g
Available Payload Volume - 97 x 97 x 53 mm3
Average Payload Power Available - 0.7 W
Available Power Buses - 3.3 V, 5 V and Battery raw
Data Rate up to 19.6 kbps

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Платформа КубСат 3U
Multi-purpose platform capable of supporting wide range of pointing, volume and power requirements

Bus Mass - 2.4-2.9 kg (configuration dependent)
Available Payload Mass - 0.5-1.6 kg (configuration dependent)
Available Payload Volume up to - 97 x 97 x 173 mm3
Average Payload Power Available - 10 W
Available Power Buses - 3.3 V, 5 V, customizable 6-12 V and Battery raw
Telemetry Data Rate - 19.6 kbps
Payload Data Rate up to - 125 Mbps

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Платформа КубСат 6U
High performance platform, easily adaptable to handle complex
Earth Observation, IoT, science, and exploration missions

Bus Mass - 4.2-4.8 kg (configuration dependent)
Available Payload Mass - 7.2-7.8 kg (configuration dependent)
Available Payload Volume - 97 x 197 x 223 mm3
Average Payload Power Available - 10-30 W (configuration dependent)
Available Power Buses - 3.3 V, 5 V, customizable 6-12 V and Battery raw
Telemetry Data Rate - 19.6 kbps
Payload Data Rate up to - 125 Mbps

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1.5U Solar Panel

Power Efficiency: ≥30%
Max Power: 3.6W
Internal By-pass diode: reverse bias protection
Solar cells thickness: 150μm ± 20μm
Sensors: Temperature and Sun (optional Gyroscope)
Available with integrated magnetorquer and RBF-pin
Max Voltage: 4.8-7.2V (for 3 cells)
Max Current: 504mA
PCB Thickness: 1.6mm
Mass: ≤65g (79g with magnetorquer)

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1U Solar Panel X/Y

Power Efficiency: ≥30%
Max Power: 2.4W
Internal By-pass diode: reverse bias protection
Solar cells thickness: 150μm ± 20μm
Sensors: Temperature and Sun (optional Gyroscope)
Available with integrated magnetorquer and RBF-pin
Max Voltage: 4.66V (for 2 cells)
Max Current: 517mA
Panel Dimensions: 82.6mm x 98mm
PCB Thickness: 1.6mm
Mass: ≤44g (53g with magnetorquer)

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3U Solar Panel

Power Efficiency: ≥30%
Max Power: 8.4W
Internal By-pass diode: reverse bias protection
Solar cells thickness: 150μm ± 20μm
Sensors: Temperature and Sun (optional Gyroscope)
Available with integrated magnetorquer and RBF-pin
Max Voltage: 16.8V (for 7 cells)
Max Current: 504mA
PCB Thickness: 1.6mm
Mass: ≤127g (155g with magnetorquer)

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6U Solar Panel

Power Efficiency: ≥30%
Max Power: 19.2W
Internal By-Pass Diode: reverse bias protection
Solar Cells Thickness: 150μm ± 20μm
Sensors: Temperature and Sun (optional Gyroscope)
MTQ: Integrated H-Bridge for control of external magnetorquer
RBF: Available with Remove Before Flight pin
Max Voltage: 19.2V (for 2x8 cells)
Max Current: 504mA
PCB Thickness 1.6mm
Mass: ≤300g

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Образовательная система космической связи
A hands-on educational kit consisting of two low-power
transceivers and a space simulation board

Feautures :
Operating Frequency Bandwidth - 430-450 MHz (physical)
Links - UHF (physical), S-band and X-band
Losses Physical Simulation - free space and additional (atmospheric, polarization etc.) losses
External Noise - interference and jamming
Frequency Compensation - Doppler effects and transceiver compensation
Configurable - Different modulation schemes, transmission speeds and packet parameters

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Патч антенна
Fully qualified X-band patch antenna

Feautures :
Frequency Range - 8025 - 8400 MHz
Half Power Beam Width (HPBW) - 74 deg
Gain - 6+ dBi over operational bandwidth
Polarization - Right Hand Circular
Mass - 2.2 g
RF Output Power up to - 4 W

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Платформа КубСат 1.5U
Flight-proven fully integrated CubeSat bus
with 30% more volume

Feautures :
Bus Mass - 1050 g
Available Payload Mass - 950 g
Available Payload Volume - 97 x 97 x 104 mm3
Average Payload Power Available - 0.9 W
Available Power Buses - 3.3 V, 5 V and Battery raw
Data Rate up to - 19.6 kbps

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NanoTorque GSW-600

Reaction wheel for nanosatellites

Main features
Long life brushless motor design
Integrated control electronics
Enclosed design
Hybrid bearings
Lubricant free
Vacuum rated
Long life
Redundant data interfaces
SPI
I2C
UART
Speed and torque control capability
Low jitter with precisely balanced flywheel

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