- Posted by doEEEt Media Group
- On October 14, 2019
More and more space missions are or are willing to use COTS EEE parts in their projects. Several working groups in ESA and outside of ESA are trying to define a standardise way to procure such type of part for space applications. This presentation will try to present the status of the different working groups’ positions and the consequence for the procurement of passive EEE parts.
NEW SPACE AND COTS
COTS components are mainly used in these applications. COTS are, today, rarely used in other types of projects except for Telecom.
New Space activities are active in:
There are three main reasons to use COTS components in space projects:
- better performances
- not existing in space QPL range
- COST, with 1/10 of the cost of equivalent space QPL parts
The first two – better performance and QPL list non-existence – are the main reasons for use in all space projects, the lower cost is the main driver for launchers and constellations applications.
Today, we have two types of space standardization systems addressing EEE parts:
- ESCC: European Procurement and qualification system (QPL and EPPL)
- ECSS: Q60 series with guidelines for selection and procurement
- Q30 and Q70 series for proper use of EEE parts
- Several other E series
All these standards would be affected by the evolution of the New Space era.
ALTER TECHNOLOGY has accumulated experience on validation of any kind of EEEcomponent putting in place a stringent methodology for product assessment, selection, procurement and testing (evaluation, screening and qualification).
doEEEt helps you to define the proper activities flow once a minimum project requirements have been set in our area "Applications expected requirements"
Space standards for procurement of commercial parts:
Can we use AEC-Q200 parts in High Rel. space?
There are several questions to be answered:
• What are the designs of the parts certified according to AEC-Q200 vs space QPL designs?
• What are the reliability data available to space customers and agencies?
• How the manufacturing processes and materials are monitored to ensure that the reliability of AEC-Q200 parts is the same that during certification (PPAP)?
• Can we accept parts without screening? If yes, for what applications?
Is the design of AEC-Q200 parts compatible?
Available reliability data?
AEC-Q200 specifies clearly the tests to be performed and the methods to be used but:
• Reliability data package of AEC-Q200 are not freely available to space customers and agencies
• How the “four corners” defined in AEC-Q200 are chosen with regards to the range of certified products?
Is PPAP assuring a stable reliability level?
For space QPL parts, we have an equivalent document that is called PID (Process Identification Document). It defines the design rules, the materials, the processes, tests and equipment used during manufacturing. BUT in addition to this, we request screening tests and a two years maintenance of qualification tests.
PPAP is generally not available for space actors. We expect that in addition to the information contained in space PID we will find some Statistical Process Control that would allow to discard regular reliability tests.
Can we accept AEC-Q200 parts for space projects?
It depends on two main aspects:
1] what are the needs and requirements?
- mission duration
- constellation or not
2] how can we trust our suppliers?
- reliability testing
What can we learn space QPL parts?
Space QPL parts are reliable. Is it too much reliable? For example, ceramic capacitors lifetime 2000 hours life test at 2 times rated voltage at 125C is equivalent to more than 100 years of operational conditions. What does it bring for a “3 years” mission? Do we still need a derating?
Screening is part of space heritage and is mandatory for flights models. It may be now the time to analyse the types of rejects during screening. Is it still relevant as it is defined?
Source: EPCI e-Symposium PCNS paper
by: Dr. Leo Farhat and Dr. Denis Lacombe; ESA ESTEC; The Netherlands
presented by D.Lacombe at the 2nd PCNS 10-13th September 2019, Bucharest, Romania as paper 3.1.
- Stability of Optoelectronic parameters for space applications - November 16, 2023
- C-SAM Ultrasonic Analysis to Identify High Voltage MLCC Defects - October 19, 2023
- SMD Inductors - October 19, 2023