Deployment System 50 kg
A non-pyrotechnic deployment system designed for 50 kg space satellites, ensuring smooth and shockless separation from the launch vehicle's upper stage.
Key figurescomparable across the catalogue
- Mass
- 4 kg
- Payload capacity
- 50 kg
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Mass
- 4.0 kg
- Max. satellite mass
- 50 kg
- Separation time
- ≤ 1 s
- Separation velocity
- 0.5 — 2.0 m/s
- Angular separation velocity
- ≤ 2 °/s
- Operating temperature
- −60°C to +60°C
About
The Deployment System 50 kg is engineered for the smooth and shockless deployment of space satellites weighing up to 50 kg. A key feature of this system is the absence of pyrotechnics, which ensures a gentle separation process at the moment the satellite detaches from the upper stage of the launch vehicle. This design minimizes potential shock loads on the satellite, contributing to its operational integrity. The system is capable of separating satellites within 1 second, with a separation velocity ranging from 0.5 to 2.0 m/s and an angular separation velocity of no more than 2 degrees per second. It is designed to operate across a wide temperature range, from -60°C to +60°C, making it suitable for the harsh conditions of space environments.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.