Reliable and Advanced Mission Injector (RAMI)
UARX Space
RAMI is an advanced satellite deployment system for CubeSats, featuring multiple actuator redundancies and an optional interface for battery charging and communication.
Typed specifications34 values
Discloses 8 of 17 fields engineers filter by in this category (category median 3).
- Capacity
- 12 U max · 1x 12U · datasheet p.2 6 U max · 1x 6U + 2x 3U | 6 U max · 2x 6U | 3 U max · 4x 3U
- Mass
- 9 kg min · configuration dependant · datasheet p.2 9 kg min · from 9.0 kg, configuration dependant
- Envelope (L×W×H)
- 330.6 mm x 383.9 mm x 448.8 mm datasheet p.2 330.6 mm x 383.9 mm x 448.8 mm external dimensions stowed (w, h, d)
- Max payload mass
- 30 kg datasheet p.2
- Actuator
- non-pyro datasheet p.2 other resettable, redundant, non-magnetic deployment actuators
- TRL
- 9 datasheet p.2
- Deployer type
- multi-slot dispenser bay configuration options 1x 12U, 2x 6U, 1x 6U + 2x 3U, 4x 3U · datasheet p.2
- Accepted satellite form factors
- 0.25U datasheet p.2 0.5U | 1U | 1.5U | 2U +3
- Satellites per form factor
- 1 12U · datasheet p.2 4 3U | 2 6U
- Max mass per satellite
- 30 kg payload · datasheet p.2 30 kg max · maximum payload mass
- Launch vehicle interface
- 5x M8 + 4x M6 (SpaceX Falcon 9 compatible) datasheet p.2
- Connector
- 1x D-Sub or individual D-Sub per each port datasheet p.2
- Random vibration
- 16 g RMS random · datasheet p.2
- Satellite class
- CubeSat datasheet p.2
- Allowed protrusion beyond the rails
- 25.5 mm nom. · maximum CubeSat side protrusions · datasheet p.2 39 mm maximum | 39 mm max · maximum CubeSat side protrusions
- Launch vehicles
- Falcon 9 datasheet p.2
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 supplier14 lines, in the manufacturer's own wording
- Supported form factors
- 0.25U, 0.5U, 1U, 1.5U, 2U, 3U, 6U, 12U
- Actuator redundancy
- Multiple redundant actuation lines
- Optional interface
- Battery charging and communication with CubeSat
- Mission orbits
- LEO and interplanetary
- Bay configuration options
- 1x 12U, 2x 6U, 1x 6U + 2x 3U, 4x 3U
- Maximum CubeSat side protrusions
- 25.5 mm nominal, and up to 39.0 mm
- Number of "Tuna can" available
- up to 5
- Maximum payload mass
- 30 kg
- Dimensions
- 330.6 mm x 383.9 mm x 448.8 mm
- Mass
- From 9.0 kg
- Mechanical fixation
- 5x M8 + 4x M6 (SpaceX Falcon 9 compatible)
- Electrical interface
- 1x D-Sub or individual D-Sub per each port
- Umbilical interface
- Charging and data port for each slot (8x 1.5 A)
- Qualification levels and status
- 16 gRMS for random, TRL9
About
The Reliable and Advanced Mission Injector (RAMI) provides advanced satellite deployment capabilities with a focus on reliability. It incorporates multiple actuator redundancies and redundant actuation lines to ensure successful deployment. An optional feature allows for an interface to charge the CubeSat’s battery and communicate with it after integration, either on the ground or during transit to its final orbit, prior to release. RAMI was designed and built with high reliability as a primary factor, making it suitable for both Low Earth Orbit (LEO) and interplanetary missions. The system is configurable to accommodate various CubeSat types, including Regular or Extra-Large lengths, supporting sizes from 0.25U up to 12U. This flexibility allows for more room for the satellite payload.
Documentation
- UARX-Q-CRE-0051-D-RAMI-ProductQuickSpecs.pdf PDF source: www.uarx.com ↗
- UARX-Q-CRE-0037-B-0.25u-QuickSpecsSheet.pdf PDF source: www.uarx.com ↗
- UARX-Q-CRE-0038-B-0.5u-QuickSpecsSheet.pdf PDF source: www.uarx.com ↗
- UARX-Q-CRE-0039-B-1u-QuickSpecsSheet.pdf PDF source: www.uarx.com ↗
- UARX-Q-CRE-0040-B-1.5u-QuickSpecsSheet.pdf PDF source: www.uarx.com ↗
- UARX-Q-CRE-0041-B-2u-QuickSpecsSheet.pdf PDF source: www.uarx.com ↗
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