Features & Benefits 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: –55ºC Performance: up to 10.3125 Gbps/lane from –40ºC to 100ºC Sensitivity: –9 dBm for BER 10–12 Low power consumption: 85 mW/lane (<10 pJ per bit)) 4 TRX (4+4)-lane per device (40G, full duplex) 12 TX or 12 RX lane 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 Internet of Space VPX single board computers High I/O density, high BW communication links Drawing of SpaceABLE SM 40 (full duplex) and 120G Dimensions are given in mm Space Qualification TestsTest 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 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. Related Videos Electrical connection with interposers Optical connection with screw-in connector Optical connection with MicroClip Optical Interconnect Design Challenges in Space Documents & Literature BrochureSpaceABLE SM Brochure622 kB Get the latest news Be the first to know! Receive straight to your mailbox the latest news on our connectivity solutions. Subscribe
Space Qualification TestsTest 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 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.
Related Videos Electrical connection with interposers Optical connection with screw-in connector Optical connection with MicroClip Optical Interconnect Design Challenges in Space