HARDWARE / PRODUCTUpdated 25 Sep 2026

Nanosatellite Platform of CubeSat 3U Format

Samara University
Nanosatellite Platform of CubeSat 3U Format

SamSat 3U CubeSat platform for scientific and technological experiments, with ~2 dm³ of payload volume.

Typed specifications5 values

Discloses 3 of 7 fields engineers filter by in this category (category median 3).

Design lifetime
1 years
product page
Lead time
12 months
product page
Form factor
3U
from product name · product page
Payload volume
2 L
product page
Flight heritage
Not flight-qualified
product page

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 supplier13 lines, in the manufacturer's own wording
Interfaces for payload connecting
CAN, I2C, SPI, UART
Voltage of payload
3.3 / 5 / 7 / 14 V
Maximum current consumption of payload
2 A
Memory of microsd card
32 GB
Contains
Onboard computer, electrical power system, transceiver, attitude stabilization system
Available payload volume
~2 dm3
Attitude stabilization angular speed
up to 0.5 deg/s
Thermal control
Passive
Year of release
2016
Design life
1 year
Lead time
12 months
Flight heritage
Not flight-qualified
Customization
Adaptable to customer requirements

About

The SamSat 3U Nanosatellite Platform, released by Samara University in 2016, is a CubeSat-format bus designed for scientific and technological experiments. It provides an onboard computer, electrical power system, transceiver and attitude stabilization system, with available payload volume of approximately 2 dm3. Payload interfaces include CAN, I2C, SPI and UART, with payload supply voltages of 3.3/5/7/14 V and a maximum payload current draw of 2 A; onboard data storage is provided by a 32 GB microSD card. The attitude stabilization system provides an angular rate of up to 0.5 deg/s, and thermal control is passive. The platform has a guaranteed service life of 1 year and an estimated production/delivery time of 12 months; it is not flight-qualified but Samara University can adapt it to customer requirements.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: trade.glavkosmos.com ↗

The rest of the range from Samara University

All 3 products →