Lyra 1
Tesseract
Lyra 1 is a bipropellant thruster designed for SmallSat propulsion subsystems, offered by Tesseract Space.
Typed specifications5 values
Discloses 4 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- chemical datasheet p.1
- Mass
- 240 g datasheet p.1
- Thrust
- 1 000 mN datasheet p.1
- Specific impulse
- 280 s max · datasheet p.1
- Min impulse bit
- 2.7 mN·s minimum · datasheet p.1
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
- Name
- Lyra 1
- Vendor
- Tesseract Space
- Subsystem
- Propulsion Subsystem
- Component type
- Bipropellant Thruster
- Form factor
- SmallSat
- Subsystem (2)
- Propulsion Subsystem
- Component type (2)
- Bipropellant Thruster
- Form factor (2)
- SmallSat
- Vendor (2)
- Tesseract Space
- Dry mass
- 0.24 kg
- Status
- In Production
About
Tesseract Space offers custom turn-key spacecraft propulsion systems, including the Lyra 1 bipropellant thruster. These systems integrate propellant tankage, plumbing, control electronics, and ancillary structure. The Tesseract team has expertise in chemical propulsion across various thrust classes and propellant types, including both storable and cryogenic propellants. The company provides flexible options for licensing and ownership of the design intellectual property, and can offer either development-only services or full development and manufacturing options. The Lyra 1 is specifically categorized as a bipropellant thruster for SmallSat form factors and is currently in production.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.