SL-OMV Space Vehicle Tug
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Key Features
- Avionics leveraging Moog鈥檚 BRE440鈩 Rad-Hard CPU
- LEO missions
- Flexible flight software is payload and mission configurable
- Green propellant propulsion system
- Single string butlayered GNC sensor suite provides resiliency
- Designed for Venture Class Launch Vehicles
Specifications
Characteristic | Performance / interfaces |
Orbital Range | 400 to 700 km |
Mission Life | < 1 years (based on propellant usage) |
Bus Mass | 70 kg Bus Dry Mass |
Bus Volume | 脴40鈥 x 25鈥 Tall with 脴24鈥 launch vehicle interface |
Orbital Position Knowledge | <5 m |
Pointing Accuracy | +/- 1 deg for deployments, +/- 10 deg for Sun Pointing |
Velocity Accuracy | 0.1 m/s |
Delta-V | Up to 200 m/s (varies with mission) |
Payload Interfaces (Mechanical) | 6x 6U CubeSats - Containerized 6x12U CubeSats 鈥 No Container |
Payload Mass | 6x 12 kg (+ 3.4 kg per Container) |
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Space
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