HARDWARE / PRODUCTAdded 9 Jul 2026

Satellite platform SXC6 modification “Basic”

SPUTNIX
Spacecraft up to 12 kg · Micro class (FAA) what this means
Satellite platform SXC6 modification “Basic”

The simplest configuration of the SXC6 6U CubeSat platform, offering only basic service systems (power, UHF comms, electromagnetic damping) to maximize available payload volume.

Typed specifications34 values

Discloses 5 of 7 fields engineers filter by in this category (category median 3).

Mass
6 kg
max · mass assembled, w/o payload, not more than · datasheet p.6
Envelope (L×W×H)
100 x 226.3 x 366
dimensions at rails, deployment system pressed · datasheet p.6
Power consumption
4.5 W
product page 60 W
Data interface
CAN
on-board interface CAN2.0 B · datasheet p.6
Operating temperature
-30–60 °C
datasheet p.6
Form factor
6U
CubeSat 6U · datasheet p.2
Orbit
LEO
payload power and solar panel figures are specified on LEO · datasheet p.6
Max payload mass
6 kg
max · max mass of payload, up to (Table 1 platform comparison) · datasheet p.2
Payload volume, U
3 U
min · 3U+, available volume for payload not less than · datasheet p.6
Payload envelope (L × W × H)
85 x 85 x 300
3U+ available volume for payload (Table 1) · datasheet p.2
Power available to payload
8 W
max · average power available to payload on LEO, Sun orientation us… · datasheet p.6 25 W max · peak (max available capacity of payload, up to; Table 1)
Regulated voltages for the payload
5 V
output voltage 5 V ±0.5 V, output current not more than 3 A · datasheet p.6
Power generation (orbit average)
35 W
min · peak on LEO, not less than; row is printed as 'Peak capacity … · datasheet p.6
Battery capacity
79 Wh
min · not less than; battery type Li-Ion 2S 5000 mAh, rated voltage… · datasheet p.6
Attitude control
3-axis stabilised
three-axis w/ reaction wheels, star tracker, magnetometer, an… · datasheet p.2
Pointing accuracy
0.1 °
orientation control accuracy on sunny and shadow side, up to … · datasheet p.6
Payload data downlink rate
57.6 kbps
max · UHF command/telemetry link, AX.25 FEC; 9600 bit/s default · datasheet p.6 10 000 kbps max · X-band downlink, DVB-S2, up to
Radio band
UHF
command radio link 435-437 MHz (amateur) or 400-401 MHz (comm… · datasheet p.6 X X-band 10.3-10.55 GHz (amateur) or 8.0-8.4 GHz (commercial), …
Subsystems included
solar arrays
deployable solar panels, included · datasheet p.2 GNSS receiver GPS-receiver, included  |  X-band downlink high-speed X-band radio link, included  |  battery Li-Ion 2S 5000 mAh, not less than 79 Wh  |  EPS regulated output voltage 5 V ±0.5 V / 3 A for payload  +2
Max satellite wet mass
12 kg
max · max mass allowed w/ payload, not more than (Table 4); Table 1… · datasheet p.6
Deployables
hinges for solar wings
deployable solar panels included · datasheet p.2
Deployables (as printed)
Deployable solar panels (included)
datasheet p.2
Satellite class
CubeSat
CubeSat nanosatellite platform line · datasheet p.2
Form factor, U (number)
6 U
CubeSat 6U · datasheet p.2

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 supplier20 lines, in the manufacturer's own wording
Outer dimensions transport mode
118.6x228.6x366 mm
Rail dimensions
100+-0.15 x 100+-0.15 x 366+-0.5 mm
Mass (w/o payload)
3.4 kg
Maximum mass
12 kg
Power supply voltage
5+-0.5 V
Power consumption
3 A
Operating temperature range
-30...+60 C
Battery type
Li-Ion 2S
Battery capacity
78 Wh
Onboard bus voltage
6.0-8.4 V (7.4 nominal)
Peak power per solar panel
not less than 15 W
Service radio frequency
435-438 or 400-401 MHz
Transmitter power
not less than 30 dBm
Receiver sensitivity
not worse than -113 dBm
Data rate
2400-57600 bps
ADCS algorithms
B-DOT
Onboard interface
CAN2.0B, SPUTNIX UniCAN
Average payload power per orbit
4.5 W
Maximum payload power
60 W
Payload volume
5U

About

The SXC6 platform is a multipurpose, combinable set of onboard service systems and structural elements for a 6U CubeSat, compatible with any payload conforming to the SXC6 ICD. The “Basic” (SXC6-VOL) modification is the simplest configuration, with minimal service systems maximizing payload volume: power supply system with battery, UHF transceiver with patch and deployable dipole antennas, and an electromagnetic angular-velocity-damping system. Supplied: assembled SXC6 platform, transportation case, USB cable, charger.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: sputnix.ru ↗

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