Single-actuation Drive. Type 1
Flight-proven electromechanical deployment drive (25 N·m, 0.75 kg, 70×94×92 mm) for solar arrays and booms. Heritage: Amos-5, KazSat-3, Express.
Technical specifications
- Purpose
- Deployment of spacecraft structure elements: solar array panels, booms, antennas
- Year of release
- 2009
- Estimated production/delivery time
- 6 months
- Flight heritage
- Amos-5, Telkom-3, KazSat-3, Express-AT1, Express-AT2, Express-AM8
- Nominal slew rate, °/s
- 2–4
- Torque rating, N·m
- 25
- Safety clutch actuation, N·m
- 50–75
- Antitorque (de-energized, N·m), not exceeding
- 2
- Operating temperature range, °C
- -50 to +60
- Operational life (cycles/hours), not less than
- 100 / 48
- Overall dimensions, mm
- 70 × 94 × 92
- Mass, kg
- 0.75
- TRL
- 9 (flight-proven)
About
The Single-actuation Drive Type 1 is an electromechanical rotary drive for deployment of large mechanical system elements including solar array panels, booms, and antennas. It provides 25 N·m torque rating at a nominal slew rate of 2–4 °/s, with a safety clutch activation threshold of 50–75 N·m and anti-torque in de-energized state of up to 2 N·m. Dimensions are 70 × 94 × 92 mm, mass 0.75 kg. Released in 2009, delivery 6 months, rated for 100 cycles / 48 hours. Flight-qualified on Amos-5, Telkom-3, KazSat-3, Express-AT1, Express-AT2, Express-AM8.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
