
- Available Payload volume:
- 97 x 97 x 53 mm
- Available Payload Mass:
- 1150 g
- Available Power:
- 700 mW (orbit and mission dependent)
- Power Buses Voltages:
- 3.3V, 5V and Battery raw
- Telemetry Data rate:
- up to 19.2 kbps
- Bus Mass:
- 850 g
- 1x Power Module
- 1x UHF Transceiver Type II
- 1x Onboard Computer
- 1x UHF Antenna
- 1x Structure 1U
- 1x Solar Panels X/Y
- 1x Solar Panels X/Y RBF
- 2x Solar Panels X/Y MTQ
- 1x Solar Panel Z
- 1x Solar Panel Z MTQ
- 2x Protoboard
- Payload integration
- Dedicated X/Y Panel with Remove-before-flight pin and system check interface
- Software drivers
- Cables
- Packed in a protective case
- Technical information (Datasheet)
- 10 hours of engineering support
- Full warranty
Our 1U CubeSat Platform is a fully integrated nanosatellite capable of supporting up to 0.5 litres (1150 grams) of scientific and commercial payload. Available with EnduroSat Attitude Determination and Control System (ADCS) for up to 3 degrees pointing accuracy and complete payload integration, this is your affordable ticket to Space. This platform has flight heritage.
Features
Included with the product
Qualification:
During the space qualification campaign, EnduroSat CubeSats underwent high level of functional tests to demonstrate the integrity of the system. All modules were performing at their nominal level. The tests were performed following the strict specifications of the ESA ECSS-E-ST-10-03C and NASA GEVS: GSFC-STD-7000A standards.
1U Cubesat Platform
EnduroSatOur 1U CubeSat Platform is a fully integrated nanosatellite capable of supporting up to 0.5 litres (1150 grams) of scientific and commercial payload. Available with EnduroSat Attitude Determination and Control System (ADCS) for up to 3 degrees pointing accuracy and complete payload integration, this is your affordable ticket to Space. This platform has flight heritage.
Features
- 1x Power Module
- 1x UHF Transceiver Type II
- 1x Onboard Computer
- 1x UHF Antenna
- 1x Structure 1U
- 1x Solar Panels X/Y
- 1x Solar Panels X/Y RBF
- 2x Solar Panels X/Y MTQ
- 1x Solar Panel Z
- 1x Solar Panel Z MTQ
- 2x Protoboard
Included with the product
- Payload integration
- Dedicated X/Y Panel with Remove-before-flight pin and system check interface
- Software drivers
- Cables
- Packed in a protective case
- Technical information (Datasheet)
- 10 hours of engineering support
- Full warranty
Qualification:
During the space qualification campaign, EnduroSat CubeSats underwent high level of functional tests to demonstrate the integrity of the system. All modules were performing at their nominal level. The tests were performed following the strict specifications of the ESA ECSS-E-ST-10-03C and NASA GEVS: GSFC-STD-7000A standards.
- Available Payload volume:
- 97 x 97 x 53 mm
- Available Payload Mass:
- 1150 g
- Available Power:
- 700 mW (orbit and mission dependent)
- Power Buses Voltages:
- 3.3V, 5V and Battery raw
- Telemetry Data rate:
- up to 19.2 kbps
- Bus Mass:
- 850 g
- 1x Power Module
- 1x UHF Transceiver Type II
- 1x Onboard Computer
- 1x UHF Antenna
- 1x Structure 1U
- 1x Solar Panels X/Y
- 1x Solar Panels X/Y RBF
- 2x Solar Panels X/Y MTQ
- 1x Solar Panel Z
- 1x Solar Panel Z MTQ
- 2x Protoboard
- Payload integration
- Dedicated X/Y Panel with Remove-before-flight pin and system check interface
- Software drivers
- Cables
- Packed in a protective case
- Technical information (Datasheet)
- 10 hours of engineering support
- Full warranty
Our 1U CubeSat Platform is a fully integrated nanosatellite capable of supporting up to 0.5 litres (1150 grams) of scientific and commercial payload. Available with EnduroSat Attitude Determination and Control System (ADCS) for up to 3 degrees pointing accuracy and complete payload integration, this is your affordable ticket to Space. This platform has flight heritage.
Features
Included with the product
Qualification:
During the space qualification campaign, EnduroSat CubeSats underwent high level of functional tests to demonstrate the integrity of the system. All modules were performing at their nominal level. The tests were performed following the strict specifications of the ESA ECSS-E-ST-10-03C and NASA GEVS: GSFC-STD-7000A standards.