SpaceABLE SM 50G and 150G radiation-resistant optical transceivers
The SpaceABLE™ SM radiation resistant transceivers are engineered to withstand radiation doses >100 krad (Si). The SpaceABLE SM embedded optical modules are rugged devices offering high bandwidth (greater than 150 Gbps) in a chip-size package.
Furthermore, all our devices are tested following ECSS process and lot acceptance testing, and component pre-screening is done for every batch of transceivers sold for this application.
Drawing of SpaceABLE SM 50 and 150G
Dimensions are given in mm.
Specifications and features
- Small: Less than 5 mm high.
- Rugged: withstand radiation doses >100 krad (Si) and qualified per MIL-STD 883 shock and vibration.
- Expected life: up to 20 years.
- Cold start temperature: –55 ºC.
- Performance: up to 12.5 Gbps/lane from –40 ºC to 100 ºC
- BER: As low as 10–15.
- Low power consumption: 85 mW/lane (<10 pJ per bit)
Please see product datasheet for detailed specifications.
- High-throughput communication satellites.
- Internet of Space.
- VPX single board computers.
- High I/O density, high BW communication links.
Radiation tests summary
Radiation Test #1:
Proton testing: Total Non-Ionizing Dose (TNID).
Testing was done at KVI – University of Groningen, The Netherlands.
Radiation Test #2:
Heavy ion testing: Single Event Effect & Latch-up (SEE and SEL).
Testing was done at Texas A&M University, USA.
Radiation Test #3:
Gamma Ray using Cobalt-60: Total Ionizing Dose (TID) (MIL-STD-883G, method 1019.7).
Testing was done at TRAD in Toulouse, France.
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.
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.