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Lessons Learned During Instrument Testing for the Thermal Infrared Sensor (TIRS)The Themal InfraRed Sensor (TIRS) instrument, set to launch on the Landsat Data Continuity Mission in 2013, features a passively cooled telescope and IR detectors which are actively cooled by a two stage cryocooler. In order to proceed to the instrument level test campaign, at least one full functional test was required, necessitating a thermal vacuum test to sufficiently cool the detectors and demonstrate performance. This was fairly unique in that this test occurred before the Pre Environmental Review, but yielded significant knowledge gains before the planned instrument level test. During the pre-PER test, numerous discrepancies were found between the model and the actual hardware, which were revealed by poor correlation between model predictions and test data. With the inclusion of pseudo-balance points, the test also provided an opportunity to perform a pre-correlation to test data prior to the instrument level test campaign. Various lessons were learned during this test related to modeling and design of both the flight hardware and the Ground Support Equipment and test setup. The lessons learned in the pre-PER test resulted in a better test setup for the nstrument level test and the completion of the final instrument model correlation in a shorter period of time. Upon completion of the correlation, the flight predictions were generated including the full suite of off-nominal cases, including some new cases defined by the spacecraft. For some of these ·new cases, some components now revealed limit exceedances, in particular for a portion of the hardware that could not be tested due to its size and chamber limitations.. Further lessons were learned during the completion of flight predictions. With a correlated detalled instrument model, significant efforts were made to generate a reduced model suitable for observatory level analyses. This proved a major effort both to generate an appropriate network as well as to convert to the final model to the required format and yielded additional lessons learned. In spite of all the challenges encountered by TIRS, the instrument was successfully delivered to the spacecraft and will soon be tested at observatory level in preparation for a successful mission launch.
Document ID
20160000799
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Peabody, Hume L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Otero, Veronica
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Neuberger, David
(Edge Space Systems Glenelg, MD, United States)
Date Acquired
January 13, 2016
Publication Date
July 14, 2013
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC-500-13-D-0067
Report Number: GSFC-500-13-D-0067
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Vail, CO
Country: United States
Start Date: July 14, 2013
End Date: July 18, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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