CONTOUR NGIMS Electronics Test History

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Presentation transcript:

CONTOUR NGIMS Electronics Test History Florence Tan Code 915/Swales Oct 29th, 2001 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

NGIMS Flight Electronics Test Summary All boards tested individually at temperature (-45C, RT, 60C) voltage (+/- 10% where applicable) Number hours assembled flight electronics tested: 400-500 at room temperature Comet encounter mass sampling strategies for closed and open sources 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

NGIMS Test Configuration Vacuum Test System – Simulates comet environment except for dust and high speed neutral gas Spacecraft Simulator Simulates spacecraft command and data handling system A PC with a 1553 I/F card Ground Support Workstation Oracle database for: Commanding functions Telemetry data repository 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

Vacuum Test System 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

NGIMS Sensor 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

NGIMS Electronics 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

NGIMS Flight Electronics Testing Testing done between July 9th - October 12th 2001 Room Temperature Phases: Ongoing V&V Ongoing Baseline Lens Tuning at Goddard Calibration at Goddard Spacecraft interface at APL 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

Testing Details – Ongoing V & V and Baseline Tests July 9th 2001 – Oct 12th 2001 Tested GSE, HW & SW using V&V SW Generated and tested instrument baseline and functional tests for verifying operation of the instrument from calibration to post-launch 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

Testing Details – Lens Tuning July 9th 2001 – September 16th 2001 To determine best lens voltages Ion source cleanup prior to gas calibration by simultaneously operating all 4 filaments Analog hardware DAC's calibrated and engineering unit conversions determined Exercised limits of high voltage amplifiers Characterized analog response times and slew rates 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

Testing Details – Calibration August 28th 2001 – September 16th 2001 Calibration closed source and open source thermally accommodated gas modes tested using single gases mass peak tuning determined using high molecular weight compound open source testing with an ion gun over energy range expected for comet encounter and flight parameter values determined for equations tested in-flight gas calibration system 500+ Baseline, characterization & calibration runs 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

Testing Details – Spacecraft Interface at APL Oct 9th, 10th, 11th 2001 Verified connector between S/C and NGIMS Powered on using S/C power Commanded NGIMS using S/C GSE Collected and verified telemetry from S/C 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

GSE Test Setup at APL 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History

CONTOUR Spacecraft / NGIMS Interface Test 10/24/2001 C:\Documents and Settings\Ftan\My Documents\NGIMS Electronics Test History