Payload Data Handling Systems

8 Payload Data Handling Systems for Space Applications from 5 manufacturers listed on SatNow

Payload Data Handling Systems for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:Payload Power and Data Handling
Space Heritage:
Yes
Orbit:
LEO
Mass:
1.1 Kg
Input Voltage:
20.5 to 25.2 V
Output Voltage:
3.8 to 23.1 V
Power Consumption:
24 to 370 W
Payload Interface:
RS-422, LVDS
Operating Temperature:
-15 to 35 Degree C
Dimension:
186 x 98 x 67 mm
Application:
Space
more info
Description:Frame Grabber Satellite Payload & Data Acquisition
Space Heritage:
yes
Mass:
0.075 Kg
Storage Capacity:
NAND Flash : 64 Gbps, DRAM : 1 Gbps
Radiation Tolerance:
30 Krad
Input Voltage:
5 or 12 V
Power Consumption:
1 W
Payload Interface:
CAN 2.0, LVDS, UART, I2C, RS422, RS485, RS232
Operating Temperature:
-40 to 85 Degree C
more info
Storage Capacity:
RAM : 1 Mb, NOR-Flash : 256 Mb, Flash : 2 Mb, SRAM : 4 Mb, FRAM : 512 kb
Payload Interface:
CAN, RS-422, SPI, USART, UART, I2C
more info
Description:Payload Data Handling System for Smallsats
Mass:
2.3 Kg
Storage Capacity:
SDRAM : 4 Gb, Flash : 16 Gb
Radiation Tolerance:
10 krad
Input Voltage:
9 to 36 V
Power Consumption:
15 W
Payload Interface:
RSS-422, RS-485, LVDS
Operating Temperature:
-20 to 70 Degree C
Dimension:
290 x 192 x 34 mm
Application:
Small Satellites
more info
Description:Payload Data Handling Unit
Storage Capacity:
1 to 4 Tb
Application:
Space-borne, Airborne
more info
Space Heritage:
Yes
Orbit:
LEO
Mass:
985 g
Storage Capacity:
1 Tb
Radiation Tolerance:
20 to 30 krad
Output Voltage:
3.3 to 23.1 V
Power Consumption:
8 W
Payload Interface:
LVDS, USB
Operating Temperature:
-20 to 40 Degree C
Dimension:
53 x 139.8 x 194.6 mm
more info
Storage Capacity:
RAM : 36 kb to 512 Mb, NOR-Flash : 32 Mb, FRAM : 512 kb
Payload Interface:
CAN, RS-422, UART, SPI, I2C, USB, LVDS, GTP, GPIO, SpaceWire
more info
Description:SmallSat Payload Power and Data Handling Unit
Space Heritage:
Yes
Orbit:
LEO
Mass:
0.780 Kg
Input Voltage:
20.5 to 25.2 V
Output Voltage:
3.8 to 23.1 V
Power Consumption:
24 to 188 W
Payload Interface:
RS-422, LVDS
Operating Temperature:
-15 to 35 Degree C
Dimension:
186 x 98 x 46 mm
Application:
Space
more info

A payload data handling system is a satellite subsystem that is designed to receive, store, process, and compress payload data (e.g., camera data) for transmission to ground stations. Satellite payloads refer to scientific instruments or equipment (e.g., telescopes, spectrometers, cameras, and particle detectors) and sensors used on a satellite to perform specific tasks. It handles real-time data processing, such as image enhancement or spectral analysis and is equipped with fault-tolerant and radiation-resistant storage systems. 

Payload data handling system is built on a FPGA or microcontroller architecture that acts as a system monitor and a communication interface with the OBC. The microcontroller also supervises the internal temperatures and internal current consumption and ensures the integrity of the memory's content. The payload data handling system is ideal for space applications, including small satellites and airborne platforms.

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