Corvus-XL
~81kg smallsat bus with electric and chemical propulsion, flown on DARPA Mandrake-2.
Typed specifications7 values
Discloses 1 of 7 fields engineers filter by in this category (category median 3).
- Mass
- 81 kg product page
- Envelope (L×W×H)
- 366 mm x 239 mm x 113 mm product page
- Power consumption
- 34 W product page
- Design lifetime
- 5 years min · LEO · product page
- Power generation (orbit average)
- 34 W as printed: power · product page
- Propulsion
- included product page
- Flight heritage
- DARPA Mandrake-2 (twin satellites, optical inter-satellite links) product page
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 supplier8 lines, in the manufacturer's own wording
- Mass
- ~81 kg
- Propulsion
- electric propulsion + monopropellant chemical thruster
- Flight heritage
- DARPA Mandrake-2 (twin satellites, optical inter-satellite links)
- Dimensions
- 366 mm x 239 mm x 113 mm
- Resolution
- 22 meter
- Data rate
- high-speed
- Lifetime
- ≥ 5 year in LEO
- Power
- 34 watts
About
Corvus-XL is a larger member of Astro Digital’s Corvus bus family, used for the DARPA Mandrake-2 mission consisting of twin satellites demonstrating optical inter-satellite links built with SA Photonics payloads. The bus carries the same 3-axis ADCS suite as other Corvus platforms plus both electric propulsion and a monopropellant chemical thruster, giving it significantly more on-orbit maneuvering capability than the smaller Corvus-Micro bus.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.