Deployment System 50 kg
KOSMOLAB Launch Services
A non-pyrotechnic deployment system designed for 50 kg space satellites, ensuring smooth and shockless separation from the launch vehicle's upper stage.
Typed specifications28 values · 28 confirmed by the manufacturer
Discloses 14 of 14 fields engineers filter by in this category (category median 1). ✓ Manufacturer-confirmed data · 2026-09
- Mass
- 4 kg ✓ manufacturer datasheet p.1
- Release time
- 2 000 ms ✓ manufacturer manufacturer
- Release shock
- 0.5 g ✓ manufacturer manufacturer
- Operating temperature
- -60 °C ✓ manufacturer product page
- TRL
- 8 ✓ manufacturer manufacturer
- Lead time
- 6–9 months ✓ manufacturer datasheet p.1
- Export status
- ITAR-free ✓ manufacturer manufacturer
- Separation type
- clamp band ✓ manufacturer manufacturer
- Interface diameter
- 200 mm ✓ manufacturer manufacturer
- Number of bolts or points
- 12 ✓ manufacturer manufacturer
- Max spacecraft mass
- 50 kg ✓ manufacturer datasheet p.1
- Max centre-of-gravity height
- 500 mm ✓ manufacturer manufacturer
- Separation velocity
- 0.5–2 m/s ✓ manufacturer manufacturer
- Tip-off rate
- 2 °/s ✓ manufacturer datasheet p.0
- Release command type
- current pulse ✓ manufacturer manufacturer
- Release actuator voltage
- 28 V ✓ manufacturer manufacturer
- Command pulse duration
- 200 ms ✓ manufacturer manufacturer
- Cycles / reuses
- 20 ✓ manufacturer manufacturer
- Satellite class
- microsat 10-100 kg ✓ manufacturer datasheet p.0
- Missions flown
- 0 ✓ manufacturer manufacturer
- Separation switches, count
- 2 ✓ manufacturer manufacturer
- Stack height
- 60 mm ✓ manufacturer manufacturer
- Release current
- 1.5 A ✓ manufacturer manufacturer
- Launch vehicles
- Angara ✓ manufacturer Angara · manufacturer PSLV PSLV✓ manufacturer | Soyuz-2 Soyuz-2✓ manufacturer | Soyuz-2.1v Soyuz-2.1v✓ manufacturer | Start-1M Start-1M✓ manufacturer
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 supplier6 lines, in the manufacturer's own wording
- 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.