Satellite platform OrbiCraft-Pro 3U modification “Experimental”
SPUTNIX
An assembled and manufacturer-verified 3U CubeSat platform (article SXC3) with silicon (Si) solar panels and basic B-DOT ADCS, intended primarily as a laboratory/educational model.
Typed specifications29 values
Discloses 4 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 1.4 kg max · mass assembled (w/o payload), not more than · datasheet p.4
- Envelope (L×W×H)
- 100x100x340.5 mm at rails (w/ deployment system pressed) · datasheet p.4 108x108x340.5 mm w/ springs pressed and antenna folded
- Supply voltage
- 5 V product page
- Data interface
- CAN on-board interface CAN2.0 B · datasheet p.4
- Operating temperature
- -30–60 °C operating temperature range · datasheet p.4
- Form factor
- 3U CubeSat 3U · datasheet p.2
- Orbit
- LEO power figures stated for LEO · datasheet p.4
- Max payload mass
- 2.6 kg max · max mass of payload, SXC3 column of Table 1 (line-level figure) · datasheet p.2
- Payload volume, U
- 1 U min · printed as "1U+" (80x70x140 mm), Table 1 · datasheet p.2
- Payload envelope (L × W × H)
- 80x70x140 mm available volume for payload, not less than (see SXC ICD) · datasheet p.4
- Power available to payload
- 0.6 W max · average power available to payload on LEO, not more than (to … · datasheet p.4 16 W max · peak (max available capacity of payload), SXC3 column of Table 1
- Regulated voltages for the payload
- 5 V nom. · output voltage 5 V ±0.5 V; output current not more than 2 A · datasheet p.4
- Battery capacity
- 39 Wh min · battery capacity, not less than; Li-Ion 2S 5000 mAh, rated 7.4 V · datasheet p.4
- Attitude control
- other B-DOT only (angular velocity sensor, magnetometer) · datasheet p.4
- Payload data downlink rate
- 9.6 kbps max · UHF radio channel 435-437 MHz, AX.25; 9600 bit/s default, 480… · datasheet p.4
- Radio band
- X high-speed X-band radio link: "Included, option" (Table 1, SX… · datasheet p.2 UHF radio channel 435-437 MHz, FM, AX.25
- Subsystems included
- battery battery capacity 39 Wh, Li-Ion 2S 5000 mAh (Table 3) · datasheet p.4 X-band downlink high-speed X-band radio link: "Included, option" (Table 1, SX… | solar arrays number of solar panels: 14 pcs. (Table 3) | OBC on-board computer SXC-MB-04 shown in SXC3 layout (Picture 2) | ADCS orientation and stabilization algorithms and sensors rows (Ta… +1
- Max satellite wet mass
- 4 kg max · max mass allowed (w/ payload), not more than · datasheet p.4
- Satellite class
- CubeSat CubeSat nanosatellite platform line · datasheet p.1 nanosat 1-10 kg nanosatellite platform line
- Form factor, U (number)
- 3 U 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 supplier18 lines, in the manufacturer's own wording
- Mass assembled (w/o payload)
- 1.4 kg
- Max mass allowed (w/ payload)
- 4 kg
- Dimensions (springs pressed, antenna folded)
- 108x108x340.5 mm
- Dimensions at rails
- 100x100x340.5 mm
- Available volume for payload
- not less than 80x70x140 mm
- Output voltage
- 5 V +-0.5 V
- Output current
- not more than 2 A
- Available average payload power on LEO
- not more than 600 mW
- Battery capacity
- not less than 39 Wh
- On-board interface
- CAN2.0 B
- Number of solar panels
- 14 pcs
- Peak power per solar panel on LEO
- not less than 0.9 W
- Operating temperature range
- -30...+60 C
- Radio channel frequency
- 435-437 MHz, FM
- Radio data rate
- 4800-56700 bit/s
- Battery type
- Li-Ion 2S 5000 mAh
- ADCS algorithms
- B-DOT
- Sensors
- Angular velocity sensor, magnetometer, temperature
About
The “Experimental” modification is an assembled/verified 3U CubeSat unit with silicon (Si) solar panels, ready for payload integration, intended primarily as a laboratory model for education. Contents: 3U CubeSat structure, on-board computer (Raspberry-Pi), power supply system with battery, twelve Si side solar panels with coils, two Si end edge solar panels with coils, UHF transceiver, UHF antenna system with service panel/RBF switch, protection panels for 3U, wiring set, transportation case, USB cable, charger, documentation. For actual missions, GaAs-panel modifications are recommended instead. Includes B-DOT ADCS algorithms and sensors: angular velocity sensor, magnetometer, and temperature sensor.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.