Renegade
12U-class nanosatellite bus with the best bus-to-payload mass ratio in the Terran Orbital line, extendable to 16U.
Typed specifications49 values
Discloses 5 of 11 fields engineers filter by in this category (category median 1).
- Mass
- 25 kg max · Launch Mass (Wet) · datasheet p.2
- Form factor, U (number)
- 12 U Configuration · datasheet p.2 16 U easily customized | 16 U option | 12 U standard point of departure | 16 U 16U option +1
- Envelope (L×W×H)
- 12U Configuration · datasheet p.2
- Supply voltage
- 3.3 V rail available · datasheet p.2 12 V Unreg | 5 V rail available
- Form factor
- 16U 16U option · datasheet p.2 12U Configuration 12U | 16U customized | 12U standard | 16U
- Orbit
- LEO Applications LEO; native orbits 400km - 1200km · datasheet p.2
- Max payload mass
- 10 kg Available Payload Mass · datasheet p.2
- Payload volume, U
- 12 U baseline · datasheet p.1 16 U option
- Regulated voltages for the payload
- 3.3 V 3.3V rail available · datasheet p.2 5 V 5V rail available | 5 V rail available
- Unregulated bus for the payload
- 12 V nom. · 12V Unreg · datasheet p.2 12 V 12V Unreg
- Power generation (orbit average)
- 100 W max · peak (Max Solar Array Power) · datasheet p.2
- Pointing accuracy
- 0.008–0.021 ° 30 to 75 arcseconds; higher accuracy available · datasheet p.2
- Propulsion
- optional None standard, options available · datasheet p.2
- Payload data downlink rate
- 2 000 kbps S-band D/L (U/L 125 Kbps) · datasheet p.2 9.6 kbps UHF (U/L & D/L) | 50 000 kbps X-Band D/L
- Radio band
- UHF datasheet p.2 S | X
- Subsystems included
- battery 12V Battery Modules (3) · datasheet p.2 EPS 12V MPPT (2), 12V Load Controller (1) | other Backplane; LDRR Radio; MDR Radio | ADCS Coarse Sensors (2), Star Trackers (2), Magnetorquers (3), Rea… | ADCS coarse sensors, star trackers, magnetorquers, reaction wheels +4
- Max satellite wet mass
- 25 kg max · Launch Mass (Wet), up to; maximum mass may not be supported o… · datasheet p.2
- Rail standard
- custom datasheet p.1
- Payload mounting
- rail based dispensers datasheet p.1
- Deployables (as printed)
- compact tri-fold solar array datasheet p.1
- Flight heritage
- Based on the previous Trestles platform, with significant heritage in orbit; based on hardware with significant flight heritage datasheet p.1
- Satellite class
- CubeSat datasheet p.0
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 supplier11 lines, in the manufacturer's own wording
- Configuration
- 12U (16U option)
- Applications
- LEO
- Native orbits
- 400 km - 1200 km
- Launch mass (Wet, max)
- Up to 25 kg
- Available payload mass
- 10 kg
- Max solar array power
- 100 W (3rd-party solar array included)
- Redundancy
- Single-string
- Power system
- 12 V Unreg, 3.3 V, 5 V rails available
- Communication data rate
- UHF: 9.6 Kbps (U/L & D/L); S-band: 125 Kbps U/L, 2 Mbps D/L; X-band: 50 Mbps D/L
- Propulsion
- None standard, options available
- Pointing accuracy
- 30 to 75 arcseconds, higher accuracy available
About
Renegade is based on the previous Trestles platform, with significant heritage in orbit, and can be easily customized as a 16U spacecraft. It shares the same avionics and GNC algorithms as the rest of Terran Orbital’s satellite line but allows more room for power storage than the other nano and microsatellite platforms. Renegade meets the requirements for ‘rail’-based dispensers, including those sold by Terran Orbital, and has a compact tri-fold solar array providing more power to a payload than what is often available in this form factor.
Key benefits: exceptional available payload volume for its size, allowing complex operational systems; platform extendable from 12U to 16U for exceptionally long payloads; can accommodate up to a 19cm diameter optical imager; based on hardware with significant flight heritage.
Baseline modules included: Flight Computer, Backplane, 12V Battery Modules (3), 12V MPPT (2), 12V Load Controller (1), Coarse Sensors (2), Star Trackers (2), GPS, Magnetorquers (3), Reaction Wheels (3), LDRR Radio, MDR Radio, IMU (1).
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.