NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
ATLAS LTCS Vertically Challenged System Lessons LearnedRe-planning of LTCS TVAC testing and supporting RTA (Receiver Telescope Assembly) Test Plan and Procedure document preparation. The Laser Thermal Control System (LTCS) is designed to maintain the lasers onboard Advanced Topographic Laser Altimeter System (ATLAS) at their operational temperatures. In order to verify the functionality of the LTCS, a thermal balance test of the thermal hardware was performed. During the first cold start of the LTCS, the Loop Heat Pipe (LHP) was unable to control the laser mass simulators temperature. The control heaters were fully on and the loop temperature remained well below the desired setpoint. Thermal analysis of the loop did not show these results. This unpredicted behavior of the LTCS was brought up to a panel of LHP experts. Based on the testing and a review of all the data, there were multiple diagnostic performed in order to narrow down the cause. The prevailing theory is that gravity is causing oscillating flow within the loop, which artificially increased the control power needs. This resulted in a replan of the LTCS test flow and the addition of a GSE heater to allow vertical operation.
Document ID
20140009179
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Patel, Deepak
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Garrison, Matt
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
July 15, 2014
Publication Date
March 25, 2014
Subject Category
Aeronautics (General)
Report/Patent Number
GSFC-E-DAA-TN13845
Report Number: GSFC-E-DAA-TN13845
Meeting Information
Meeting: Spacecraft Thermal Control Workshop
Location: El Segundo, CA
Country: United States
Start Date: March 25, 2014
End Date: March 27, 2014
Sponsors: Aerospace Corp.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Loop Heat Pipe
xxxx
xxxx
No Preview Available