Deployer 12U 2×6U
The Deployer 12U 2×6U enables simultaneous deployment of two 6U-class CubeSats, compatible with various launch vehicles and customizable to specific requirements.
Typed specifications36 values · 35 confirmed by the manufacturer
Discloses 16 of 17 fields engineers filter by in this category (category median 3). ✓ Manufacturer-confirmed data · 2026-09
- Capacity
- 6 U ✓ manufacturer datasheet p.1 12 U 2x6U configuration✓ manufacturer
- Mass
- 9 kg ✓ manufacturer datasheet p.1
- Envelope (L×W×H)
- 480 × 290 × 299 mm ✓ manufacturer datasheet p.1
- Max payload mass
- 26 kg ✓ manufacturer datasheet p.1
- Separation velocity
- 0.5–2 m/s ✓ manufacturer manufacturer
- Actuator
- spring ✓ manufacturer manufacturer
- Operating temperature
- -60 °C ✓ manufacturer min · datasheet p.1 60 °C max✓ manufacturer
- TRL
- 9 ✓ 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.1
- Accepted satellite form factors
- 6U ✓ manufacturer datasheet p.1 6U 6U✓ manufacturer
- Satellites per form factor
- 2 ✓ manufacturer 6U · datasheet p.1
- Max mass per satellite
- 12 kg ✓ manufacturer 6U · manufacturer
- Rail and interface standard
- CDS rev.14 ✓ manufacturer manufacturer
- Tuna-can volume (diameter × height)
- 80 х 40 ✓ manufacturer manufacturer
- Tip-off rate
- 2 °/s ✓ manufacturer datasheet p.1
- 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
- flight-qualified as part of the Angara-A5 launch vehicle (2024 launch) ✓ manufacturer datasheet p.3
- Satellite class
- CubeSat ✓ manufacturer datasheet p.1
- Missions flown
- 1 ✓ manufacturer manufacturer
- Quasi-static load
- 10 g ✓ manufacturer manufacturer
- Release current
- 2 A ✓ manufacturer manufacturer
- Allowed protrusion beyond the rails
- 6.5 mm ✓ manufacturer manufacturer
- Launch vehicles
- Angara ✓ manufacturer manufacturer Soyuz-2.1v Soyuz-2.1v✓ manufacturer | Soyuz-2✓ manufacturer | PSLV✓ manufacturer | Start-1M✓ manufacturer
- Indicative price
- 5 500 000 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)
- 480 × 290 × 299 mm
- Mass
- 9 kg
- Max. satellite mass
- 26 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
- 2 × CubeSat 6U
About
The KosmoLab Deployer 12U 2×6U is designed for the simultaneous deployment of two 6U-class CubeSats. This deployer is compatible with a range of launch vehicles, including Angara, Soyuz/Fregat, PSLV, and Start-1M. Customization options are available to precisely match the specific requirements of your CubeSat and the chosen launch vehicle. Key specifications include dimensions of 480 × 290 × 299 mm (L×W×H), a mass of 9 kg, and a maximum satellite mass capacity of 26 kg. It boasts a separation time of less than or equal to 1 second, with a separation velocity ranging from 0.5 to 2.0 m/s and an angular separation velocity of less than or equal to 2 °/s. The deployer operates effectively within a temperature range of −60°C to +60°C.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.