OrbiCraft-Pro 3U CubeSat Platform
SPUTNIX
Spacecraft up to 4 kg · Nano class (FAA) what this means
3U CubeSat satellite platform / assembly kit. The "Flight" (SXC3-GA) version is factory-assembled and tested with GaAs solar panels. Variants: Experimental (SXC3), Flight (SXC3-GA), Pro (SXC3-GA-ADC) with enhanced attitude control.
Typed specifications45 values
Discloses 5 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 2.2 kg max · SXC3-ADC; mass assembled (w/o payload), not more than; value … · datasheet p.4 1.4 kg max · SXC3-AS (basic); mass assembled (w/o payload), not more than | 2.2 kg max · SXC3-GA3-ADC; mass assembled (w/o payload), not more than; va… | 1.45 kg max · SXC3-GA3-AS; mass assembled (w/o payload), not more than
- Envelope (L×W×H)
- 100x100x340.5 mm all SXC3 modifications; at rails (w/ deployment system pressed) · datasheet p.4 108x108x340.5 mm all SXC3 modifications; w/ springs pressed and antenna folded
- Data interface
- CAN all SXC3 modifications; on-board interface CAN2.0 B · datasheet p.4
- Operating temperature
- -30–60 °C all SXC3 modifications; operating temperature range · datasheet p.4
- Form factor
- 3U all SXC3 modifications; CubeSat 3U · datasheet p.2
- Orbit
- LEO all SXC3 modifications; power figures stated for LEO · datasheet p.4
- Max payload mass
- 2.6 kg max · all SXC3 modifications; max mass of payload, SXC3 column of T… · datasheet p.2
- Payload volume, U
- 1 U min · all SXC3 modifications; printed as "1U+" (80x70x140 mm), Table 1 · datasheet p.2
- Payload envelope (L × W × H)
- 80x70x140 mm all SXC3 modifications; available volume for payload, not les… · datasheet p.4
- Power available to payload
- 16 W max · all SXC3 modifications; peak (max available capacity of paylo… · datasheet p.2 0.2 W max · SXC3-ADC; average power available to payload on LEO, Sun orie… | 0.6 W max · SXC3-AS (basic); average power available to payload on LEO, n… | 2 W max · SXC3-GA3-ADC; average power available to payload on LEO, Sun … | 1.5 W max · SXC3-GA3-AS; average power available to payload on LEO, not m…
- Regulated voltages for the payload
- 5 V nom. · all SXC3 modifications; output voltage 5 V ±0.5 V; output cur… · datasheet p.4
- Battery capacity
- 39 Wh min · all SXC3 modifications; battery capacity, not less than; Li-I… · datasheet p.4
- Attitude control
- 3-axis stabilised SXC3-ADC; three-axis w/ reaction wheels, magnetometer, angula… · datasheet p.2 other SXC3-AS (basic); B-DOT only (angular velocity sensor, magneto… | 3-axis stabilised SXC3-GA3-ADC; three-axis w/ reaction wheels, magnetometer, an… | other SXC3-GA3-AS; B-DOT only (angular velocity sensor, magnetometer)
- Pointing accuracy
- 5 ° max · SXC3-ADC; orientation control accuracy, shadow side · datasheet p.4 1 ° max · SXC3-ADC; orientation control accuracy, sunny side | 5 ° max · SXC3-ADC; orientation setting accuracy, shadow side | 1 ° max · SXC3-ADC; orientation setting accuracy, sunny side | 5 ° max · SXC3-GA3-ADC; orientation control accuracy, shadow side +3
- Payload data downlink rate
- 9.6 kbps max · all SXC3 modifications; UHF radio channel 435-437 MHz, AX.25;… · datasheet p.4
- Radio band
- X all SXC3 modifications; high-speed X-band radio link: "Includ… · datasheet p.2 UHF all SXC3 modifications; radio channel 435-437 MHz, FM, AX.25
- Subsystems included
- battery all SXC3 modifications; battery capacity 39 Wh, Li-Ion 2S 500… · datasheet p.4 X-band downlink all SXC3 modifications; high-speed X-band radio link: "Includ… | solar arrays all SXC3 modifications; number of solar panels: 14 pcs. (Tabl… | OBC all SXC3 modifications; on-board computer SXC-MB-04 shown in … | ADCS all SXC3 modifications; orientation and stabilization algorit… +1
- Max satellite wet mass
- 4 kg max · all SXC3 modifications; max mass allowed (w/ payload), not mo… · datasheet p.4
- Satellite class
- CubeSat all SXC3 modifications; CubeSat nanosatellite platform line · datasheet p.1 nanosat 1-10 kg all SXC3 modifications; nanosatellite platform line
- Form factor, U (number)
- 3 U all SXC3 modifications; CubeSat 3U · 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 supplier14 lines, in the manufacturer's own wording
- Form factor
- 3U CubeSat
- Mass (without payload)
- 1.4 kg
- Max mass (with payload)
- 4 kg
- Dimensions
- 108 × 108 × 340.5 mm
- Payload volume
- 80 × 70 × 20 mm
- Solar cells
- 14
- Battery
- Li-Ion 2S 5000 mAh, ≥ 39 Wh
- Supply voltage
- 7.4 V nominal
- Payload power (orbit-avg)
- ≥ 600 mW
- Radio
- 435–437 MHz, AX.25 / FEC, 4800–56700 bit/s
- ADCS
- B-DOT + gyro & magnetometer sensors
- Bus interface
- CAN 2.0B
- Operating temperature
- −30 … +60 °C
- Variants
- SXC3, SXC3-GA, SXC3-GA-ADC
About
3U CubeSat satellite platform / assembly kit. The “Flight” (SXC3-GA) version is factory-assembled and tested with GaAs solar panels. Variants: Experimental (SXC3), Flight (SXC3-GA), Pro (SXC3-GA-ADC) with enhanced attitude control.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.