Deployer 16U
The Deployer 16U is designed for the deployment of a single 16U-class spacecraft, compatible with various launch vehicles including Angara, Soyuz/Fregat, PSLV, and Start-1M.
Typed specifications37 values · 36 confirmed by the manufacturer
Discloses 17 of 17 fields engineers filter by in this category (category median 3). ✓ Manufacturer-confirmed data · 2026-09
- Capacity
- 16 U ✓ manufacturer datasheet p.1
- Mass
- 12 kg ✓ manufacturer datasheet p.1
- Envelope (L×W×H)
- 600 × 290 × 299 mm ✓ manufacturer product page
- Max payload mass
- 40 kg ✓ manufacturer datasheet p.1
- Separation velocity
- 2 m/s ✓ manufacturer max · product page 0.5–2 m/s✓ manufacturer
- Actuator
- spring ✓ manufacturer manufacturer
- Operating temperature
- -60 °C ✓ manufacturer min · datasheet p.1 60 °C max✓ manufacturer
- TRL
- 7 ✓ manufacturer manufacturer
- Lead time
- 6–9 months ✓ manufacturer indicative · manufacturer
- Export status
- ITAR-free ✓ manufacturer manufacturer
- Deployer type
- tube (P-POD type) ✓ manufacturer datasheet p.0
- Accepted satellite form factors
- 16U ✓ manufacturer datasheet p.0 16U 16U✓ manufacturer
- Satellites per form factor
- 1 ✓ manufacturer 16U · datasheet p.0
- Max mass per satellite
- 40 kg ✓ manufacturer 16U · datasheet p.0
- Max satellite envelope
- 226.3 x 226.3 x 454 ✓ manufacturer 16U · manufacturer
- Rail and interface standard
- CDS rev.14 ✓ manufacturer manufacturer
- Tuna-can volume (diameter × height)
- 80 х 40 ✓ manufacturer 16U · manufacturer
- Tip-off rate
- 2 °/s ✓ manufacturer datasheet p.0
- Launch vehicle interface
- M6, 8 bolt ✓ manufacturer manufacturer
- Release command type
- voltage pulse ✓ manufacturer manufacturer
- Release actuator voltage
- 28 V ✓ manufacturer manufacturer
- Command pulse duration
- 200 ms ✓ manufacturer manufacturer
- Flight heritage
- Angara-A5 launch vehicle (2024 launch) ✓ manufacturer datasheet p.3
- Satellite class
- CubeSat ✓ manufacturer datasheet p.0
- Missions flown
- 0 ✓ manufacturer manufacturer
- Quasi-static load
- 10 g ✓ manufacturer manufacturer
- Release current
- 2 A ✓ manufacturer manufacturer
- Allowed protrusion beyond the rails
- 6.5 mm ✓ manufacturer 16U · manufacturer
- Launch vehicles
- Angara ✓ manufacturer manufacturer Soyuz-2.1v Soyuz-2.1v✓ manufacturer | Soyuz-2✓ manufacturer | PSLV✓ manufacturer | Start-1M✓ manufacturer
- Indicative price
- 6 000 000 EUR min · 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 supplier8 lines, in the manufacturer's own wording
- Dimensions (L×W×H)
- 600 × 290 × 299 mm
- Mass
- 12 kg
- Max. satellite mass
- 40 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
- Payload
- 1 × CubeSat 16U
About
The KosmoLab Deployer 16U is engineered for the precise and reliable deployment of a single 16U-class spacecraft. This deployer is compatible with a range of prominent launch vehicles such as Angara, Soyuz/Fregat, PSLV, and Start-1M, ensuring broad mission applicability. KosmoLab offers customization options to tailor the deployer to the specific requirements of your spacecraft, providing flexibility for diverse mission profiles. Key specifications include compact dimensions of 600 × 290 × 299 mm and a mass of 12 kg. It can accommodate a maximum satellite mass of 40 kg, with a rapid separation time of less than or equal to 1 second. The separation velocity ranges from 0.5 to 2.0 m/s, and the angular separation velocity is maintained at less than or equal to 2 °/s. The deployer is designed to operate effectively across a wide temperature range, from −60°C to +60°C.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.