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Technical Paper

International Space Station Automated Safing Responses to Hazardous Atmosphere

2004-07-19
2004-01-2549
Environmental Control and Life Support (ECLS) system functionality aboard the International Space Station (ISS) includes responding to various emergency conditions. The ISS requirements define three types of emergencies: fire, rapid depressurization, and hazardous or toxic atmosphere. The ISS has automatic integrated vehicle responses to each of these emergencies. These automated responses are designed to aid the crew in their response actions to the emergencies. The response to a hazardous atmosphere on board the ISS, including the automatic integrated vehicle response and crew actions, is the focus of this paper. Philosophies regarding the detection of and response to emergencies involving chemical releases are described. Vehicle configuration is discussed for currently supported automatic responses, and crew actions are defined for modules on orbit up to the addition of the Docking Compartment (DC1) in the assembly sequence.
Technical Paper

International Space Station Metal Oxide Odor Anomaly

2004-07-19
2004-01-2598
On occasion, seemingly normal operations can have significant effects upon the closed environment of the International Space Station (ISS). An example of such a case occurred on February 20, 2002 when a nominal Metal Oxide (MetOx) canister regeneration operation onboard the ISS resulted in an unexpected, foul odor that affected the crew and station operations. A case study summarizing the root cause for the event and steps taken to ensure that future MetOx regeneration operations proceed safely is presented. Included in the summary are engineering analyses and environmental monitoring results supporting the root cause assessment as well as testing conducted and flight operations changes implemented to ensure safe operations.
Technical Paper

Performance Assessment of the Exploration Water Recovery System

2008-06-29
2008-01-2140
A new water recovery system architecture designed to fulfill the National Aeronautics and Space Administration's (NASA) Space Exploration Policy has been tested at the Marshall Space Flight Center (MSFC). This water recovery system architecture evolved from the current state-of-the-art system developed for the International Space Station (ISS). Through novel integration of proven technologies for air and water purification, this system promises to elevate existing system optimization. The novel aspect of the system is twofold. First, volatile organic compounds (VOC) are removed from the cabin air via catalytic oxidation in the vapor phase, prior to their absorption into the aqueous phase. Second, vapor compression distillation (VCD) technology processes the condensate and hygiene waste streams in addition to the urine waste stream. Oxidation kinetics dictate that removing VOCs from the vapor phase is more efficient.
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