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Space photonics · technical draft

5 W space optical booster and preamplifier systems

Combined optical power amplification and receive preamplification in a compact mission enclosure.

Platform specification; mission evidence required

  • 5 W listed booster output
  • Combined booster and preamplifier
  • 30 krad reported radiation rating

This platform combines transmit-side power amplification with a low-noise receive function. The listed power and radiation figures describe the platform reference, while the delivered configuration and mission acceptance require separate confirmation.

Configuration options

Each row is a separate configuration. Limits from different rows must not be combined.
Platform referenceListed booster outputReported radiation rating
Combined space amplifier5 WUp to 30 krad; conditions to confirm

Technical details

Reference orbit class
LEO design context
Signal wavelength
Confirm the exact passband of this platform
Receive amplifier gain and noise
Not numerically specified
Radiation conditions
Material reference, shielding, dose rate and particle environment not specified

Integration and delivery

Integration
Shared mission enclosure; dimensions, mass, power and thermal path to confirm

Conditions and configuration notes

  • Mission acceptance requires a configuration-specific qualification plan and evidence for the delivered hardware. No blanket flight, radiation or standards qualification is asserted by this draft.
  • Review thermal-vacuum, vibration, shock, radiation and electromagnetic requirements with the mission interfaces.
  • The 30 krad figure is not a complete radiation qualification. Its test method, dose basis and applicability to the delivered configuration must be reviewed.

Applications to discuss

  • LEO optical terminals
  • Spaceborne transmit and receive chains

Specify your configuration

Precisometer supports selection and integration. Contact us for a quotation against an agreed configuration.

  • Target wavelength or passband and input/output power
  • Gain, noise, timing and polarization requirements
  • Optical connections, control interface and installation conditions
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Space photonics and ground-station systems →

Local technical draft · configuration and final specifications require confirmation.