Space-EP-LEO-satellites

One of the more exciting aspects of the emerging new space market is the launch of high-volume low-Earth-orbit (LEO) satellites that are small and economically feasible, but also radiation-tolerant and reliable. These satellites enable expanded communication and connectivity around the world. Unlike the traditional satellite market, where the majority of missions are in geosynchronous orbit up to 22,236 miles from Earth and expected to last more than 10 years, LEO satellites orbit much closer to Earth, not more than 1,300 miles away. Because they’re relatively easy to replace, they generally have mission lives for less than seven years.

The major challenges in electronic design for LEO satellites – all while meeting strict budgets and maintaining competitiveness – are:

  • Using smaller, more integrated components to reduce board size.
  • Finding devices with short lead times for quick-turn designs.
  • Having electronic components capable of enduring the harsh conditions in space.


New Space Enhanced Plastic (Space EP) portfolio

integrated circuit icon Meet LEO satellite needs with radiation-assured plastic ICs in our new Space Enhanced Plastic portfolio

TI recently launched a new Space Enhanced Plastic (Space EP) portfolio of products, in addition to its current portfolio of more than 250 Qualified Manufacturers List Class V (QMLV) hermetic-space-grade devices. The Space EP portfolio comprises plastic devices designed for LEO satellites with short mission lives.

For designers new to the space market, there are specific challenges in space that products designed for terrestrial markets do not address, including:

  • Radiation performance.
  • Controlling process and material variations typical in commercial off-the-shelf (COTS) devices.
  • Thermal cycling as satellites move around Earth.
  • Outgassing from plastic packages, which are not hermetically sealed.

TI’s Space EP qualification process addresses these challenges and removes the need for high-risk upscreening methods sometimes used for this market. Upscreening is the practice of testing a part electrically or environmentally for use outside of datasheet specifications. Upscreening without a full understanding of the “recipe” of a device and its test vectors can lead to field failures and a false sense of security that the satellite will function for the mission duration.

How radiation-assured plastic devices reduce risk

TI’s certified space products enable designers and component engineers to design and qualify their boards without worrying about the specific considerations of satellites in an LEO space environment. Some of the considerations that Space EP products address are:

  • A controlled baseline flow. TI manufactures each Space EP device at a single fabrication facility, assembly site and test site in order to control site-to-site variations between material set, radiation tolerance and electrical specifications.
  • Radiation lot acceptance testing. Space EP devices are tested for total ionizing dose (TID) assurance to 20 krad (Si) for each wafer lot, removing any risk of radiation variation from lot to lot. The devices are characterized to a 30-krad(Si) TID during qualification for extra radiation performance. (For programs that require a higher level of TID performance, TI’s traditional QMLV space products are generally rated to 100 krad(Si) or higher.)
  • Gold wire. Space EP devices use only gold bond wires, eliminating the bond integrity and reliability issues possible with copper given tighter tolerance requirements.
  • No risk of tin whiskering. Tin whiskering, even when using a conformal coating, is a concern because of the harsh conditions in space. To avoid this risk, Space EP products do not use terminations with high tin content. Instead, finishes are either nickel-palladium-gold or 63% tin/37% lead.
  • Extended temperature range. Space environments typically require a temperature tolerance of -55°C to 125°C. Qualifying Space EP parts to this temperature range eliminates the need to upscreen for an extended temperature range, which would invalidate TI’s warranty and potentially harm devices used in flight.
  • Harsh environment qualifications. Space EP products receive additions to the flow specific to the space environment with extended high accelerated stress testing, temperature cycling on every device and an enhanced material set, to meet the NASA-driven American Society for Testing and Materials E-495 outgassing specification.

Accelerate launch timelines

The quality and reliability in TI Space EP devices enables designers to spin and qualify new designs faster. Within the device product folder on TI.com, we provide all radiation data for the device, optimized for LEO requirements, as well as outgassing data and reliability reports. Using our detailed reports can be a huge cost saver since a significant investment is made in radiation testing, upscreening and accounting for low yield when using COTS products in LEO satellite applications.

Our reports include:

  • A radiation report provided for TID, including characterization data for 30 krad(Si) and radiation-hardness assured data to 20 krad(Si)
  • A radiation report for single-event effects, a single-event latchup report to 43 MeVcm2/mg and additional single-event transient characterization for power-management products.
  • An outgassing and reliability report that provides information about product flow, reliability data, traceability and outgas testing. The information in this report helps expedite board qualification and reduces the need for external qualification efforts, minimizing risk when selecting new products and giving you confidence that the devices will work from the beginning.

Table 1 lists the six Space EP devices in our portfolio, with more planned in the major functional categories.

Product

Websites

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TL7700-SEP supply-voltage supervisor

Data sheet
Radiation reports

TL7700CMPWTPSEP

TPS73801-SEP 1-A low-noise, fast transient response low-dropout regulator

Data sheet
Radiation reports

TPS73801MDCQTPSEP

TLV1704-SEP 2.2-V-to-36-V radiation-hardened microPower quad comparator

Data sheet
Radiation reports

TLV1704AMPWPSEP

INA240-SEP 80-V, low- or high-side zero-drift current-sense amplifier with enhanced pulse-width modulation rejection

Data sheet
Radiation reports

INA240PMPWTPSEP

SN55HVD233-SEP 3.3-V Controller Area Network transceiver with standby mode

Data sheet
Radiation reports

SN55HVD233MDTPSEP

SN65C1168E-SEP dual differential drivers and receivers with ±8-kV International Electrotechnical Commission electrostatic discharge protection

Data sheet
Radiation reports

SN65C1168EMPWSEP

Table 1: Released Space EP devices

For projects that require qualification to a higher level of reliability or radiation assurance than the Space EP portfolio, TI continues to invest in and offer its portfolio of traditional space products in hermetic packaging.

Additional resources

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