Satellite platform SXC6 modification "Basic"

Satellite platform SXC6 modification "Basic"

Article: SXC6-VOL

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The SXC6 nanosatellite platform is a multipurpose, combinable set of onboard service systems and structural elements for the development of a small satellite in the CubeSat 6U format. It is possible to install any payloads, compatible with SXC6 ICD.

SXC6-VOL is the most simple platform configuration which contains very basic minimum of service systems, while has the maximum payload volume. This modification has the following systems:

•  PSS with battery

•  UHF transceiver with patch and deployable dipole antennas

• electromagnetic system of angular velocity damping

 

*Standard modification. Can be changed for particular project.

 

Contents:

• SXC6 platform assembled

• Transportation case

• USB cable

• Charger

 

Options included::

  • AS - Assembling and verification on manufacturer site
  • TFF - Basic functional testing with protocol: PSU cycling, radio channel, electromagnetic angular velocity damping test

 

 Available options:

• MGM - a remote sensor unit of increased accuracy (magnetometer, AVS) to improve the accuracy of the ADCS.

 Additional services:

• SXC6-TM - mechanical and thermal vacuum tests with SXC6 special equipment. The price is fixed for 1 spacecraft.

• SXC6-PLR - design review of the payload (study of the electrical circuit in terms of interfaces, software and 3D model). The price is estimated individually.

• SXC6-PLI - integration of PN: mechanical (brackets), electrical (cables, power supply), informational (interface adapters, software revision). The price is estimated individually.

• SXC6-FL - preparation of 1 spacecraft for launch: certificates for GK LS, fixing of connections, etc.

 

 

Parameters

General parameters

Outer dimensions  in transportation mode  nominal, mm

118.6x228.6x366 

Rail dimensions (with separation springs pressed-in) in transportation mode, mm

100±0,15 х 100±0,15 x 340,5±0,5 

Outer dimensions in deployed mode, mm

118.6x228.6x366 

Mass (w/o payloads), no more than, kg

3,4

Maximum mass,  no more than, kg

12 

Power supply voltage, V

5 V ±0.5 V

Power consumption, no more than, A

PC connection interface

micro-USB, WiFi

Operational temperature range

-30...+60 °С

Power supply system

Battery type

Li-Ion 2S

Battery capacity, W*h

78 

Onboard bus voltage, V

6.0..8.4V (7.4 V – nominal)

Max battery current, A

10

Peak power per solar panel, not less, W

15

Battery type

2S+2P

Service radio channel

Type

Two-way, space-Earth, Earth-space

Service radio frequency, MHz

435-438 MHz or 400-401 MHz (on request)

Redundancy

Dublicated

Telemetry

  • Radio beacon with service systems and payload telemetry. 
  • On-demand extended telemetry for each system.
  • Payload data.

Modulation type

Frequency modulation

Transmitter power, not less, dBm

30 

Receiver sensitivity, not worse, dBm

-113 

Protocol

AX.25, USP (with using FEC)

Data rate, bps

57600, 38400, 19200, 9600  (default), 4800, 2400

Antenna 1 type 

Deployable

Polarization 1

Linear

Antenna 1 gain, dBi

ADCS

ADCS algorithms

B-DOT

Sensors

Angular velocity sensor, Magnetometer, temperature sensors

Payload interface

Onboard interface

CAN2.0 B

Onboard protocol

SPUTNIX UniCAN

Average payload power per orbit, W

4,5 W

Maximum payload power consumption,W

60 

Payload volume

5U

Payload PCB slots

8

Payload PC/104 slots 

2

Payload standard cable connections

14

Payload power channels  

22

Ask more info

See more

Satellite platform SXC6 modification "ADC"

SXC6-ADC

Price on request