APPENDIX AVI212 Spezifikationen PDF herunterladen (Seite 64)

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GAIA.ASU.SP.ESM.00007

Issue 2.00

Page 64 of 79

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GAIA.ASU.SP.ESM.00007 (Avionics SCOE Req Iss 2).doc

3.12 Avionics SCOE Validation Test

Avionics SCOE validation testing is defined as the process of verifying the functionality of the SCOE, with

particular regard to meeting the specified requirements at the Spacecraft Interfaces.

Thus, a successful validation test gives confidence that the SCOE can be connected to the Spacecraft and

perform with expected results.

AVI-3363/GSE-SYS-411/T,R

The Avionics SCOE supplier shall provide an automated test solution for validating the Avionics

SCOE, which fulfils the following minimum objectives:

• Proves the Spacecraft Interfaces meet the specifications herein provided.

• Verifies the Interfaces to the RTS and CCS.

AVI-3364/CREATED/A,R

To achieve this, the supplier shall utilise existing resources wherever possible, such as:

• Using stimulation interfaces to verify measurement interfaces (and vice versa).

• Using loopback techniques (to verify BUS, RS422 links etc.)

AVI-3844/CREATED/R

All tools, test aids, cables and test stubs required to perform Avionics SCOE validation shall be

delivered with the SCOE.

AVI-3845/CREATED/R

All associated costs for providing the Avionics SCOE Validation facility, including hardware, software

and development costs, shall be provided in a separate Work Package (WP) of the subcontractor's

proposal.

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