Multipurpose Satellite Platform
Beyond Gravity (ex-RUAG Space)
Payload-agnostic 150-250 kg LEO platform with electric propulsion, ~1 kW power, low-drag profile and stackable multi-launch configuration.
Typed specifications10 values
Discloses 2 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- electric Electric Propulsion · datasheet p.2
- Mass
- 150–250 kg product page
- Design lifetime
- 7 years nom. · ~7 years lifetime in LEO · datasheet p.2 7 years in Low Earth Orbit (LEO)
- Orbit
- LEO Versatile LEO Satellite Platform · datasheet p.1
- Payload envelope (L × W × H)
- 1000 x 170 x 470 Internal Payload Bay; external payloads outside the bay also … · datasheet p.2
- Power generation (orbit average)
- 1 000 W min · printed 'Designed with 1'000 W power and more'; orbit average… · datasheet p.2
- Propulsion
- included Electric Propulsion · datasheet p.2
- Subsystems included
- propulsion Electric Propulsion · datasheet p.2
- Max satellite wet mass
- 150–250 kg nom. · nominal mass incl. payload, printed '150-250 kg and beyond' (… · 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 supplier7 lines, in the manufacturer's own wording
- Total mass
- 150-250 kg
- Power
- Designed with 1 kW and more
- Design life
- Approximately 7 years in LEO
- Internal payload bay
- 1000 mm x 170 mm x 470 mm
- Additional payload volume
- In +Z and -Y directions
- Propulsion
- Electric propulsion
- Launch configuration
- Stackable for multi-launch; compatible with heritage and new small launchers
About
Beyond Gravity offers an adaptable satellite platform for Low Earth Orbit that ensures efficient payload accommodation with scalable power and propulsion, packed within a low drag profile for longer lifetime in orbit.
Key features include a payload agnostic design, electric propulsion, a simple and cost-efficient platform configuration, compatibility with heritage and with new small launchers, a design for multi launch (stackable) configuration, and competitive and flexible launch scheduling.
The platform is designed for approximately 7 years of lifetime in Low Earth Orbit, with a total mass of 150-250 kg, 1 kW power and more, an internal payload bay of 1000 mm x 170 mm x 470 mm and additional payload volume in +Z and -Y.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.