Products
Satellite Payload
The products for QKD satellite payloads are characterized by their modularity. This allows the use of very different satellite platforms. The subsystems of the payload are compactly designed and have all common interface standards to the satellite bus.
A satellite payload contains the following major subsystems:
- FPS (Faint Pulse Source)
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MOSM (Memory System)
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MGU (Management Einheit)
Satellite payload QSS1
Name | Number | Size per unit/ mm³ |
Mass per unit/ kg | Parameter | Specification |
---|---|---|---|---|---|
FPS | 2 | 200x200x300 | 12 | Repetition Rate DV QKD Wave lengh |
2 GHz or 5 GHz BB84 protocol 850nm |
QRNG | 2 | Integrated into FPS | See FPS | Data Rate | 1 Gbit/s |
MOSM | 1 | 200x300x400 | 2 | Memory capacity | 4 TByte or 8 TByte |
MMU | 1 | 200x300x250 | 1 | Processor | TBC |
LCT | 1 | See datacheet | 15 | Aperture CPA elevation & azimut |
80mm 105° 320° |
Satellite | 1 | TBC | TBC | Pointing accuracy Rotation rate Power average Power nom. |
Better than 1° Max. 0,2°/s 20W 120W |
The QSS1 payload is currently under development. Delivery of the first flight models will take place from August 2026.
Satellite payload QSS2
Name | Number | Size per unit/ mm³ |
Mass per unit/ kg | Parameter | Specification |
---|---|---|---|---|---|
FPS | 2 | 200x200x300 | 12 | Repetition Rate DV QKD Wave lengh |
2 GHz or 5 GHz BB84 protocol 850nm |
QRNG | 2 | Integrated into FPS | See FPS | Data Rate | 1 Gbit/s |
MOSM | 1 | 200x300x400 | 2 | Memory capacity | 4 TByte or 8 TByte |
MMU | 1 | 200x300x250 | 1 | Processor | TBC |
LCT | 1 | See datacheet | 15 | Aperture CPA elevation & azimut |
80mm 105° 320° |
Satellite | 1 | TBC | TBC | Pointing accuracy Rotation rate Power average Power nom. |
Better than 1° Max. 0,2°/s 20W 120W |
Faint Pulse Source Systems
MO-SPACE offers space qualified FPS systems. The systems are characterized by very high repeating rates, which guarantee high key rates.
The following modules are offered:
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Faint Pulse Source M500
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Repetition rate max. 500MHz
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Faint Pulse Source G2
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Repetition max. 2 GHz
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Faint Pulse Source G5
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Repetition max. 5 GHz
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The systems are under development. Space qualification will be completed in early 2025.