SpaceABLE 10G SM Series 4TRX, 12TX, and 12RX

SpaceABLE 10G SM Series radiation-resistant optical transceivers

The SpaceABLE® 10G SM Series radiation-resistant onboard embedded optical transmitter and receiver modules offer radiation hardness, robustness, longevity, and high I/O density. The SpaceABLE line of products with their intrinsic radiation resistance, are well suited to provide optical interconnect within space vehicles. These devices are extremely rugged and deliver bandwidth in excess of 120 Gbps in a chip size part. 

These modules are offered as a (4+4)-lane transceiver, a 12-channel transmitter, or a 12-channel receiver. All modules operate at 10.3125 Gbps per channel over a recommended operating temperature range of –40 ºC to 85 ºC at ultra-low bit error rates of 10-12.  SpaceABLE 10G SM Series radiation resistant transceivers are engineered to withstand radiation doses >100 krad (Si). Furthermore, all our devices are tested following ECSS process and lot acceptance. Component pre-screening can be done for every batch of transceivers sold for this application.

Drawing of SpaceABLE 10G SM Series
Dimensions are given in mm.

Radiation resistant

Specifications and features

  • Small: Less than 6  mm high (SMT version)
  • Rugged: withstand radiation doses >100 krad (Si) and qualified per MIL-STD 883 shock and vibration.
  • Expected life: up to 20 years.
  • Performance: up to 10.3125 Gbps/channel over a recommended operating temperature range of –40 ºC to 85 ºC
  • Sensitivity: –9 dBm for BER 10–12
  • Low power consumption: 85 mW/channel  (<10 pJ per bit)
  • 4 TRX (4+4)-lane per device (40G, full duplex)
  • 12 TX or 12 RX channel per device (120G)
  • Multimode 850 nm wavelength laser
  • Standard MT parallel fiber connector
  • Surface mountable or pluggable
  • RoHS or tin-lead
  • Monitoring: LOS, RSSI, temperature, etc

Applications

  • High-throughput communication satellites
  • LEO satellite constellations
  • GEO satellites (with extended lifetime option)
  • Board-to-board and payload-to-payload connections
  • High I/O density, high BW communication links
A datasheet is available

A datasheet is available for this product.
Please use the "Contact" button to request it.

Space qualification tests summary

  • Proton testing: Total Non-Ionizing Dose (TNID)
  • Heavy ion testing: Single Event Effect & Latch-up (SEE and SEL)
  • Gamma Ray using Cobalt-60: Total Ionizing Dose (TID)
  • Random vibration: NASA GEVS, GSFC-STD-7000A
  • TVAC: Vacuum < 5E-5 hPa
  • Outgassing: ECSS-Q-ST-70-02C

SpaceABLE also passed standard LightABLE qualifications

  • Vibration tests per MIL-STD-883, Method 2007.3.
  • Mechanical shock tests per MIL-STD-883, Method 2002.4.
  • Thermal shock tests per MIL-STD-883, Method 1011.9.
  • Damp heat tests per MIL-STD-202, Method 103B.
  • Cold storage tests per MIL-STD-810, Method 502.5.
  • Thermal cycling tests per MIL-STD-883, Method 1010.8.

References

Stephen Buchner, Paul Marshall, Scott Kniffin and Ken LaBel. “Proton testing guidelines”, NASA/Goddard Space Flight Center, 2002.
Doug Sinclair and Jonathan Dyer. “Radiation Effects and COTS Parts in SmallSats”, SSC, 2013.