Refine Your Search

Search Results

Author:
Viewing 1 to 6 of 6
Technical Paper

Extravehicular Mobility Unit (EMU)/International Space Station (ISS) Coolant Loop Failure and Recovery

2006-07-17
2006-01-2240
Following the Colombia accident, the Extravehicular Mobility Units (EMU) onboard ISS were unused for several months. Upon startup, the units experienced a failure in the coolant system. This failure resulted in the loss of Extravehicular Activity (EVA) capability from the US segment of ISS. With limited on-orbit evidence, a team of chemists, engineers, metallurgists, and microbiologists were able to identify the cause of the failure and develop recovery hardware and procedures. As a result of this work, the ISS crew regained the capability to perform EVAs from the US segment of the ISS Figure 1.
Technical Paper

Selection of an Alternate Biocide for the ISS Internal Thermal Control System Coolant - Phase II

2004-07-19
2004-01-2472
The ISS (International Space Station) ITCS (Internal Thermal Control System) includes two internal coolant loops that utilize an aqueous based coolant for heat transfer. A silver salt biocide had previously been utilized as an additive in the coolant formulation to control the growth and proliferation of microorganisms within the coolant loops. Ground-based and in-flight testing demonstrated that the silver salt was rapidly depleted, and did not act as an effective long-term biocide. Efforts to select an optimal alternate biocide for the ITCS coolant application have been underway and are now in the final stages. An extensive evaluation of biocides was conducted to down-select to several candidates for test trials and was reported on previously.
Technical Paper

International Space Station Internal Thermal Control System Cold Plate/Fluid-Stability Test - Two Year Update

2003-07-07
2003-01-2518
Operation of the Internal Thermal Control System (ITCS) Cold Plate/Fluid-Stability Test Facility commenced on September 5, 2000. The facility was intended to provide advance indication of potential problems on board the International Space Station (ISS) and was designed: To be materially similar to the flight ITCS. To allow for monitoring during operation. To run continuously for three years. During the first two years of operation the conditions of the coolant and components were remarkably stable. During this same period of time, the conditions of the ISS ITCS significantly diverged from the desired state. Due to this divergence, the test facility has not been providing information useful for predicting the flight ITCS condition. Results of the first two years are compared with flight conditions over the same time period, showing the similarities and divergences.
Technical Paper

Selection of an Alternate Biocide for the International Space Station Internal Active Thermal Control System Coolant Loops

2003-07-07
2003-01-2568
The International Space Station (ISS) IATCS (Internal Active Thermal Control System) includes two internal coolant loops that use an aqueous based coolant for heat transfer. A silver salt biocide was used initially as an additive in the coolant formulation to control the growth and proliferation of microorganisms in the coolant loops. Ground-based and in-flight testing has demonstrated that the silver salt is rapidly depleted and not effective as a long-term biocide. Efforts are now underway to select an alternate biocide for the IATCS coolant loop with greatly improved performance. An extensive evaluation of biocides was conducted to select several candidates for test trials.
Technical Paper

The Application of Grab and Time Integrated Sampling to the Characterization of Trace Contaminants Contributed by the Docking and Integration of the Priroda Module to Space Station Mir

1998-07-13
981744
The docking and integration of the Priroda module into the Space Station Mir Complex in 1996 provided a unique opportunity to assess the potential impact on the trace contaminant concentrations in the station complex. Since Priroda was substantially loaded with new US flight hardware, the data are potentially relevant to future similar operations associated with the buildup of the International Space Station. Grab samples were collected to assess the Priroda concentrations prior to integration and to capture the profile of concentrations after the start of Priroda inter-module ventilation. A long term time integrated sampler was configured for collection of canister samples over a time interval of seven days.
Technical Paper

Determination of Organic Carbon and Ionic Accountability of Various Waste and Product Waters Derived from ECLSS Water Recovery Tests and Spacelab Humidity Condensate

1992-07-01
921313
Development testing of the Space Station Freedom (SSF) Water Recovery and Management Subsystem is being conducted by the Marshall Space Flight Center Environmental Control and Life Support (ECLS) Branch and the Boeing Missiles and Space Division. The testing program is designed to define integrated subsystem performance, one aspect of which is assessing the quality of the waste and product waters. Recent efforts have focused on maximizing the characterization of water contaminants to more fully account for the total organic carbon and ionic conductivity of the various waste and product waters. Total organic carbon accountability improved with the application of new analytical methods for certain classes of water soluble compounds. Methods developed for the detection of aldehydes, glycols, and low-level total organic carbon are discussed.
X