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The Norris-Landzberg equation is that it is required by ECSS in many calculations. For example, ECSS-Q-ST-70-61 and several ESA Memos indicate that the use of this equation is mandatory in order to assess if the qualification perform of PBAs covers the environment of the mission. Similar methodologies are widely referenced in MIL and NASA standards
Discover how Apogee Semiconductor enhances space mission reliability through radiation-immune products and scalable fault containment architectures — enabling cost-effective, system-level resilience from ground to orbit.
DACs convert processed digital data into analog signals for space systems, with designs hardened against radiation effects.
Data conversion in space systems relies on ADCs to digitize analog signals, balancing resolution, speed, and radiation tolerance.
Analog to digital converters for space must balance high resolution with low sampling rates to ensure accurate signal capture.
Solid state relays offer fast, durable switching for space systems but must be assessed for radiation sensitivity.
Single Event Latch-up protection uses current limiters to prevent damage from ionizing particles in space applications.
ASIC design focuses on custom integrated circuits for specific functions, with added complexity for space applications.
Electrical test of operational amplifiers monitors key parameters to assess performance under space-related stress conditions.
Explore evolving definitions of rad-hard components and how radiation effects shape semiconductor selection in modern satellite systems.
Explore rad-hard, enhanced, and commercial strategies for satellite design and how each balances cost, risk, and radiation resilience.
This article explores five SRAM memory design approaches for achieving a 16 Mbit memory bank in space systems, comparing traditional...
Rad-hard Schottky diodes from STMicroelectronics offer ESCC-qualified options for high-reliability space power applications.
Data Device Corporation (DDC) has compiled a list of frequently asked questions related to its EEPROM family.
Overload protection in satellite PDUs uses LCLs to monitor current and safely disconnect loads during fault conditions.
External visual inspection ensures EEE parts quality by identifying critical features and common issues in FPGAs and components per MIL-STD-883 Method 2009.
Space-grade SSD solutions combine NAND flash and radiation-tolerant controllers to ensure data integrity in harsh space environments.
Low Voltage Differential Signaling (LVDS) enables high-speed, low-power data transmission with strong noise immunity and low EMI.
In this webinar, you will gain a deeper understanding of the NX product roadmap, which is fully dedicated to Space.
DDC’s 1Mb EEPROM, listed on ESA’s EPPL, ensures high reliability, radiation performance, and ease of integration.