This case study examines how a leading commercial satellite operator achieved exceptional reliability in their Earth observation constellation using Mxtronics high-reliability components.

Customer Background: The customer operates a constellation of 24 small satellites in Low Earth Orbit (LEO) for commercial Earth imaging. Each satellite carries a high-resolution imaging payload requiring precision data acquisition and reliable power management. The constellation provides daily coverage of the entire Earth's surface for agricultural, environmental, and commercial customers.

The Challenge: The customer faced several technical challenges for their imaging payload: First, the data acquisition system needed 16 channels of precision analog input with 16-bit resolution to capture high-quality image data from the sensor array. Second, the system had to operate reliably in the radiation environment of LEO (estimated 30-50 krad(Si) over 5-year mission life). Third, power consumption had to be minimized to maximize imaging time per orbit given limited solar panel capacity. Fourth, the tight satellite integration schedule required components with short lead times and comprehensive technical support.

The Solution: LiTong recommended a complete Mxtronics solution for the imaging payload data acquisition system. The design used four MXD1604 16-bit SAR ADCs to provide 16 channels of precision acquisition with 500 kSPS sampling rate per channel. Eight MXPGA816 programmable gain amplifiers provided flexible signal conditioning with gain programmable from 0.5 to 128, allowing optimization for different sensor types. Power management used redundant MXD5303 triple-output DC-DC converters with MXLDO33 LDO post-regulators for clean analog power. All components were radiation-tolerant versions rated for 100 krad(Si) TID, providing margin over the mission requirement.

Implementation: LiTong's FAE team provided comprehensive support throughout the design process. Initial architecture review confirmed the solution met all technical requirements. Schematic review identified optimal component placement and routing for noise minimization. Layout review ensured proper grounding, decoupling, and thermal management. The customer completed the design and built engineering models for qualification testing.

Qualification Results: The data acquisition system underwent comprehensive qualification testing including: Thermal vacuum testing (TVAC) with 500 cycles between -35°C and +60°C, vibration testing to launch levels per NASA-STD-7003, and radiation testing with TID exposure to 50 krad(Si) (mission requirement) plus margin. All testing was completed successfully with the system meeting specifications before, during, and after environmental exposure.

On-Orbit Performance: The constellation was launched over a 12-month period. After more than 3 years of on-orbit operation, the data acquisition systems have achieved 99.9% availability with zero component failures. The precision acquisition has enabled image quality exceeding customer requirements, with signal-to-noise ratio 23% better than specification. The low power consumption of the Mxtronics solution allowed the customer to increase imaging duty cycle by 15% compared to their original design, increasing revenue-generating capacity.

Customer Feedback: The customer's Chief Engineer reported: 'The Mxtronics solution exceeded our reliability expectations while delivering the precision we need for high-quality Earth imaging. The radiation tolerance and low power consumption were critical to our mission success. LiTong's technical support throughout design and qualification was exceptional.' The customer has since standardized on Mxtronics components for their next-generation satellite program.