Партнеры

Солнечная панель 1U Z

КПД: ≥30%
Максимальная мощность: 2,4 Вт
Встроенный By-Pass диод: защита от обратного смещения
Толщина солнечной ячейки: 150 мкм ± 20 мкм
Датчики: температуры и солнца (опционально гироскоп)
Опционально комплектуется магнитоторкером
Совместимость с UHF-антенной EnduroSat
Максимальное напряжение: 4,8 В (для 2 ячеек)
Максимальный ток: 504 мА
Толщина печатной платы: 1,6 мм
Масса: ≤48 гр. (57,5 гр. с магнитоторкером)

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CUBESENSE

Fine Sun or Earth Sensor

CubeSense is a CMOS-based Sun and Earth sensor with a wide field of view, low power usage and high accuracy. CubeSense is a highly compact, single sensor head with integrated electronics.

These sensors provide Sun/Earth measurements with <0.2° (3σ) accuracy over a 180° field of view. The sun sensors are completely immune to albedo effects, making them highly robust and versatile. All sensors are calibrated in our state-of-the-art dark calibration room, using a sun simulator and highly accurate rotation stage. CubeSense has flight heritage for a wide variety of missions and orbits.

In orbit since 2014

Physical
Mass - 30g
Operating temperature - -20°C to 70°C
Vibration - 14g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3
Average power - 100mW
Peak power - 200mW
Communications - I2C/UART

Performance
Accuracy (3-sigma) - <0.2° with Earth/Sun fully in view
Update rate - 2Hz
FOV - 180°

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CubeWheel Large
Small Satellite Reaction Wheels
Physical
Mass - 225g
Dimensions - 57x57x31.5mm
Operating temperature - -10°C to 60°C
Vibration - 8.9g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 350mW
Peak power - 4.5W
Communications - I2C/UART/CANPerformance
Speed range - ±6000
Momentum @ max speed - 30.61mNms
Max torque - 2.3mNm
Static imbalance - <0.006 g·cm
Dynamic imbalance - <0.05 g·cm
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CubeWheel Medium
Small Satellite Reaction Wheels
Physical
Mass - 150g
Dimensions - 46x46x31.5mm
Operating temperature - -10°C to 60°C
Vibration - 8.9g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 190mW
Peak power - 2.3W
Communications - I2C/UART/CANPerformance
Speed range - ±6000
Momentum @ max speed - 10.82mNms
Max torque - 1mNm
Static imbalance - <0.004 g·cm
Dynamic imbalance - <0.014 g·cm
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CUBEWHEEL Small+
Small Satellite Reaction Wheels
Physical
Mass - 90g
Dimensions - 33.4x33.4x31.5mm
Operating temperature - -10°C to 60°C
Vibration - 8.9g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 190mW
Peak power - 2.3W
Communications - I2C/UART/CANPerformance
Speed range - ±6000
Momentum @ max speed - 3.6mNms
Max torque - 2.3mNm
Static imbalance - <0.004 g·cm
Dynamic imbalance - <0.014 g·cm
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CubeWheel Small
Small Satellite Reaction Wheels
Physical
Mass - 60g
Dimensions - 28x28x26.2mm
Operating temperature - -10°C to 60°C
Vibration - 14g RMS
Radiation - 24kRadElectrical
Supply voltage - 3V3 & 6.4-16V
Average power (2000 rpm) - 150mW
Peak power - 0.65W
Communications - I2C/UART/CANPerformance
Speed range - ±8000
Momentum @ max speed - 1.77mNms
Max torque - 0.23mNm
Static imbalance - <0.003 g·cm
Dynamic imbalance - <0.005 g·cm
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CHAMELEON IMAGER
HIGH-PERFORMANCE CHAMELEON CAMERA SYSTEMS FOR CUBESATS

CHAMELEON - MS
Spatial resolution (GSD) at 500 km - PAN 10 m; MS 20 m
Swath at 500 km - 40 km
Mass (Including electronics) - 1.6 kg
Spectral bands - 7 × MS
Satellite Bus Size - Compatible with 3U or 6U
Physical Size - 2 U (10 cm × 10 cm × 20 cm excl. electronics)
(10 cm × 10 cm × 21.5 cm with rear-mounted CU)
Flight Heritage - Flight Model Hyperspectral delivered for 2020 launch
Data format - 8-bit or 16-bit
Integrated mass data storage - 128 Gigabytes
Compression - RAW or J2K lossless or lossy
Data interface - LVDS, SPI, I2C, CAN, RS422
Power Usage - imaging mode: < 10 W; readout mode: < 5 W
Power Supply - 5V DC
Operating temperature - +10˚C to +30˚C
Survival Temperature - -20˚C to +70˚C
Radiation Tolerance (TID) - Tested to 30k Rad

CHAMELEON - HS
Spatial resolution (GSD) at 500 km - Binned to 20 m or 40 m
Swath at 500 km - 20 km
Mass (Including electronics) - 1.6 kg
Spectral bands - 148 × HS
Satellite Bus Size - Compatible with 3U or 6U
Physical Size - 2 U (10 cm × 10 cm × 20 cm excl. electronics)
(10 cm × 10 cm × 21.5 cm with rear-mounted CU)
Flight Heritage - Flight Model Hyperspectral delivered for 2020 launch
Data format - 8-bit or 16-bit
Integrated mass data storage - 128 Gigabytes
Compression - RAW or J2K lossless or lossy
Data interface - LVDS, SPI, I2C, CAN, RS422
Power Usage - imaging mode: < 10 W; readout mode: < 5 W
Power Supply - 5V DC
Operating temperature - +10˚C to +30˚C
Survival Temperature - -20˚C to +70˚C
Radiation Tolerance (TID) - Tested to 30k Rad

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NanoPower P31u

Electrical Power Supply system for small nanosatellites

Main Features
Optimal for 1U and 2U platforms
Battery voltage 8V
20 Wh battery onboard
Photovoltaic power conversion up to 30 W
ISS launch compliant version available
Key functionality
3 input channels with independent power point setting
Three different photovoltaic power point options
Battery under-voltage and over-voltage protection
Two regulated power buses
6 user-controlled output switches w. latching current limiter
Discrete control of output switches
Onboard housekeeping measurements
Interface to battery board NanoPower BP4 and BPX
Separation-switch interface with latching mechanism
Remove-Before-Flight-pin interface
Onboard lithium ion battery pack
Onboard microcontroller with I2C interface
CSP network protocol for seamless integration with other GomSpace products

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3U Powerpack

Complete power system for 3U-nanosatellite

The 3U Power Pack includes a power supply, battery pack and full solar panel set for a 3U nanosatellite:

1 NanoPower P31uS
1 NanoPower BP4
1 NanoPower P110UA
1 NanoPower P110UB
1 NanoPower P110UC
1 NanoPower P110A
1 NanoPower P110B
1 NanoPower P110C
4 NanoPower P110AS
4 NanoPower P110BS
Power Harness
Main features:
Photovoltaic power up to 60 W
Two regulated power buses: 3.3V@5A and 5V@4A
Up to six 3.3V@3A outputs
Up to six 5V@3A outputs
Battery capacity: 2600-5200 mAh

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NanoPower BP4

Small and powerful battery module for CubeSats

Feautures :
18650 Li-Ion cells with a nominal capacity of 2600 mAh
Two configurations are available:
2P-2S: 6 - 8.4 V & 5.2 Ah
1P-4S: 12 - 16.8 V & 2.6 Ah
Integrated temperature sensors with digital interface
Battery heater
Auxiliary MOSFET switch (e.g. to drive thermal knives for deployables)
Stackable for increased capacity
Fits standard PC104
ISS launch compliant version availabl

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NanoMind A3200

Versatile On-board Computer for Cube, Nano and Microsat missions

Feautures :
High-performance AVR32 MCU with advanced power saving features
512 KB build-in flash
128 MB NOR flash (On two dies of 64 MB each)
32 kB FRAM for persistent configuration storage
32 MB SDRAM
RTC clock
On-board temperature sensors
Interfaces:
I2C, UART, CAN-Bus
8 external ADC channels that can also be used as GPIO
External SPI with 3 chip selects
Cubesat Space Protocol (CSP)
GOSH interface for check-out
Attitude control system features:
3-Axis magneto resistive sensor
3-Axis gyroscope
3 bidirectional PWM outputs with current measurements
I2C interface for GomSpace Sensor Bus (GSSB)
Electrical features:
2 x 20-position hard-gold plated FSI one-piece connector

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Высокопроизводительная система для наблюдения за Землёй
High performing Camera-system for Earth Observation Projects

Feautures :
Integrated System:

Industrial Lens
3-megapixel color sensor
Advanced data processing and storage on-board
Image Acquisition:

1/2" (4:3) format color CMOS sensor
2048 x 1536 pixels
10-bit RGB Bayer pattern
Lens Performance (for each lens version):

8 mm lens: <260 m/pixel from 650 km
35 mm lens: <60 m/pixel from 650 km
70 mm lens: <30 m/pixel from 650 km
400-750 nm spectral transmission
Data Processing:

High performance ARM processor
512 MB on-board DDR2 RAM
2 GB solid state image storage
RAW, BMP and JPEG output format
Interface:

CSP-enable CAN, I2C and TTL level serial interfaces
Serial port with text-based console for debugging
Mechanical Features:

Standard PC/104 size, 96 mm x 90 mm
Mass: from 169 g with the 8 or 35 mm lens
Mass: from 277 g with the 70 mm lens

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