Skip to main content

Miniaturization of Satellite Technology Advancements

Key Takeaways

  • Advancements in miniaturization significantly reduce the costs of developing and launching satellites, allowing for faster deployment typically under two years.
  • Effective thermal management, power optimization, compact communication systems, and radiation hardening are crucial in the miniaturization process.
  • CubeSats, small standardized satellites, have been pivotal in this growth, providing cost-effective solutions for Earth observation, environmental monitoring, and technological testing.

CubeSats are a type of miniature satellite that is gaining in popularity

CubeSats are a type of miniature satellite that is gaining in popularity. 

Historically, the costs associated with developing satellites have been exceptionally high, particularly for larger GEO satellites, which often exceed 500 kg. However, with advancements in the miniaturization of satellite technology, the expenses for both development and launch can be significantly reduced. Organizations now repurpose powerful processors, adapting them to endure the harsh conditions of space. This approach is not only more cost-effective but also speeds up the process of getting satellites into orbit as they can be designed, manufactured, and launched more quickly and cost-effectively, typically in under two years.

Engineering Considerations in Miniaturization of Satellite Technology

Consideration

Description

Thermal Management

  • Develop effective solutions to dissipate heat and maintain stable operating temperatures in the compact space of a satellite. 
  • Ensure temperature-sensitive components are not placed next to components that generate significant heat in orbit.

Power Management

  • Optimize power generation and storage systems to ensure a reliable power supply within the limited space available.

Communication Systems

  • Design compact and efficient communication systems to balance high data rates with the constraints of limited space and power.

Structural Integrity

  • Use lightweight yet durable materials and construction techniques to withstand the stresses of launch and the harsh conditions of space.

Radiation Hardening

  • Implement radiation-hardened components or protective shielding to ensure electronics can withstand space radiation.

Modularity and Standardization

  • Adopt modular and standardized components for simplified design, assembly, maintenance, and upgrades.

Reliability Testing

  • Conduct rigorous environmental and reliability testing to ensure all components and systems function as required in space, especially if using off-the-shelf components.

Mass Constraints

  • Recognize that the space industry is more constrained by mass than by volume, requiring careful selection and optimization of components to minimize weight.

Industry Trends for Miniaturization of Satellite Technology

The satellite industry has seen significant growth in the deployment of small satellites, particularly in the 1–50 kg range, driven by advancements in miniaturization. The number of nano satellites and micro satellites launched annually has risen sharply, with projections estimating over 500 small satellites launched between 2015 and 2019, generating a market value of approximately $7.4 billion. 

The U.S. Department of Defense has also shifted towards procuring smaller satellites due to their resilience and reduced vulnerability to targeting. This transition reflects a broader industry trend toward leveraging the advantages of small satellite constellations for enhanced data collection and communication capabilities. 

Usage and Capabilities of Different Sized Satellites

Satellite Size

Mass Range (kg)

Usage

Capabilities

Femto Satellites

< 0.1

Educational purposes, technology demonstrations, basic research

Limited by size, used for testing new technologies, swarm missions for distributed sensing

Pico Satellites

0.1 to 1

Educational projects, simple experiments, technology validation

Small sensors and communication devices, low cost and ease of deployment

Nano Satellites

1.1 to 10

Academic research, Earth observation, communication

More complex missions, multiple instruments, higher data rates, CubeSats common for LEO missions

CubeSats

1 to 10

Educational, research, commercial missions, Earth observation

Standardized nanosatellites, cost-effective, rapid deployment, wide range of applications

Micro Satellites

10 to 200

Scientific missions, commercial applications, military uses

Heavier payloads, advanced imaging systems, robust communication links, detailed monitoring

Mini Satellites

201 to 600

Earth observation, communication networks, scientific research

High-resolution data, multiple instruments, meteorology, remote sensing, global communication

Small Satellites

601 to 1,200

Comprehensive commercial, scientific, defense missions

Detailed Earth observation, secure communications, sophisticated payloads and systems

Medium to Extra Heavy

1,201 to >7,000

Major commercial telecom, high-res Earth observation, defense

Highest payload capacity, geostationary communications, global navigation, detailed measurements

CubeSats

CubeSats, typically around 10 centimeters per side and weighing about 1.4 kilograms, have been instrumental in this growth. These small satellites, often deployed from the International Space Station, have applications in humanitarian, environmental, and commercial fields. For instance, CubeSats are being used to provide daily images of Earth, aiding in monitoring crop health, tracking carbon emissions, and urban planning. 

Additionally, NASA's CubeSat-compatible Compact Thermal Imager (CTI) has captured millions of infrared images to monitor wildfires and agricultural health. The space station's role in deploying these satellites has provided an accessible and affordable platform for testing new technologies, fostering innovation, and expanding the small satellite industry.

Modularity and Reliability in Mini Satellites

Small satellites often have shorter lifetimes (e.g., micro or small satellites have a lifetime of 5 years compared to 15 years for traditional large satellites). Additionally, these satellites often use modular designs and standardized components, which enhances their flexibility and reduces costs. 

Specifically, the use of commercial off-the-shelf (COTS) components is common in small satellite design, which can lead to lower costs, but also poses challenges in ensuring the reliability and durability of these components in the harsh space environment. This can lead to higher failure rates and shorter lifespans for satellites using these components. As COTS components may not be designed to withstand the harsh conditions of space, such as radiation, extreme temperatures, and vacuum, this necessitates additional testing and sometimes modifications to ensure their suitability for space applications.

Allegro X Features For Satellite Miniaturization

Features

Explanation

Features in Allegro X

Aids in Miniaturization of Satellite Technology

Embedded Components within PCB Design

Embedding components within the PCB rather than mounting them on the surface. 

Allegro X supports designing with embedded components through comprehensive library and schematic capabilities, ensuring accurate placement and connectivity.

Aids in Miniaturization: Embedding components reduces the overall board size and height, allowing for more compact and lightweight satellite designs essential for space constraints.

High-Density Interconnect (HDI)

HDI technology uses finer lines and spaces, smaller vias, and higher connection pad density.

Allegro X provides advanced HDI design capabilities, including via-in-pad, micro-vias, and stacked vias, enhancing routing density and signal integrity.

HDI technology allows for more components and connections in a smaller area, crucial for the miniaturization of complex satellite systems.

MTBF (Mean Time Between Failures)

MTBF is a measure of the predicted reliability and lifespan of electronic components. 

Part of Allegro X System Capture for reliability, includes MTBF analysis tools that calculate based on MIL-HDBK-217F and FIDES standards. Users can configure specific environmental and operational parameters for accurate predictions .

Aids in Miniaturization: Ensuring high MTBF in compact designs reduces the risk of failure in space, where repairs are impossible, thus enhancing the reliability of miniature satellites.

Electrical Overstress (EOS)

Electrical overstress occurs when a component is subjected to voltages or currents beyond its maximum rating, leading to potential failure. 

Part of Allegro X System Capture for reliability, provides electrical stress analysis by calculating power dissipation, voltage, and current for each component, and generates stress derating reports. Users can also configure and adjust stress settings to match specific design requirements.

Preventing EOS through accurate stress analysis allows for the use of smaller, more efficient components without compromising reliability. This is crucial for maintaining the performance and longevity of miniature satellites, which operate in harsh environments and have limited space for cooling mechanisms.

As the miniaturization of satellite technology continues to revolutionize space missions, designers face the challenge of creating compact, reliable, and efficient systems. Cadence offers powerful tools like Allegro X to help streamline this process. With Allegro X, you can leverage advanced capabilities to ensure your miniaturized satellites meet the highest standards. Explore how PCB Design and Analysis Software from Cadence can enhance your satellite design.

Leading electronics providers rely on Cadence products to optimize power, space, and energy needs for a wide variety of market applications. To learn more about our innovative solutions, talk to our team of experts or subscribe to our YouTube channel.