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Flight Testing of the Capillary Pumped Loop 3 ExperimentThe Capillary Pumped Loop 3 (CAPL 3) experiment was a multiple evaporator capillary pumped loop experiment that flew in the Space Shuttle payload bay in December 2001 (STS-108). The main objective of CAPL 3 was to demonstrate in micro-gravity a multiple evaporator capillary pumped loop system, capable of reliable start-up, reliable continuous operation, and heat load sharing, with hardware for a deployable radiator. Tests performed on orbit included start-ups, power cycles, low power tests (100 W total), high power tests (up to 1447 W total), heat load sharing, variable/fixed conductance transition tests, and saturation temperature change tests. The majority of the tests were completed successfully, although the experiment did exhibit an unexpected sensitivity to shuttle maneuvers. This paper describes the experiment, the tests performed during the mission, and the test results.
Document ID
20030025293
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ottenstein, Laura
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Butler, Dan
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cheung, Kwok
(Naval Research Lab. Washington, DC, United States)
Baldauff, Robert
(Naval Research Lab. Washington, DC, United States)
Hoang, Triem
(TTH Research, Inc. Capitol Heights, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Space Technology and Applications Forum
Location: Albuquerque, NM
Country: United States
Start Date: February 2, 2003
End Date: February 6, 2003
Distribution Limits
Public
Copyright
Public Use Permitted.
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