Satellite platform OrbiCraft-Pro 3U modification “Profi”
SPUTNIX
An assembled and manufacturer-verified 3U CubeSat platform (article SXC3-GA-ADC) with GaAs solar panels and a triaxial ADCS with reaction wheels and sun sensors, suitable for laboratory use and low-Earth-orbit flight.
Typed specifications33 values
Discloses 5 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 2.2 kg max · mass assembled (w/o payload), not more than; value printed in… · 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
- 2 W max · average power available to payload on LEO, Sun orientation, n… · 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
- 3-axis stabilised three-axis w/ reaction wheels, magnetometer, angular velocity… · datasheet p.2
- Pointing accuracy
- 5 ° max · orientation control accuracy, shadow side · datasheet p.4 1 ° max · orientation control accuracy, sunny side | 5 ° max · orientation setting accuracy, shadow side | 1 ° max · orientation setting accuracy, sunny side
- 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 supplier14 lines, in the manufacturer's own wording
- Mass assembled (w/o payload)
- 1.45 kg
- Max mass allowed (w/ payload)
- 4 kg
- Dimensions (springs pressed, antenna folded)
- 108x108x340.5 mm
- Available volume for payload
- not less than 80x70x140 mm
- Output voltage
- 5 V +-0.5 V
- Available average payload power on LEO
- not more than 1500 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 2 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
About
The “Profi” modification is an assembled/verified 3U CubeSat unit with GaAs solar panels and triaxial ADCS, ready for payload integration, usable as a laboratory model or in orbit. Contents: 3U CubeSat structure, on-board computer (with sensors and ADC controller), power supply system with battery, twelve GaAs side solar panels with coils, two GaAs end edge solar panels with coils, UHF transceiver, UHF antenna system with service panel/RBF switch, a reaction wheels module, five sun sensors, protection panels for 3U, wiring set, transportation case, USB cable, charger, documentation. Pre-flight tests and spacecraft preparation not included.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.