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Featured researches published by Daniel J. Leonard.
41st International Conference on Environmental Systems | 2011
Ryan N. Schaezler; Anthony J. Cook; Daniel J. Leonard; Ahmed Ghariani
The International Space Station (ISS) overboard leakage of cabin atmosphere is continually tracked to identify new or aggravated leaks and to provide information for planning of nitrogen supply to the ISS. The overboard leakage is difficult to trend with various atmosphere constituents being added and removed. Changes to nitrogen partial pressure is the nominal means of trending the overboard leakage. This paper summarizes the method of the overboard leakage trending and presents findings from the trending.
international conference on evolvable systems | 2004
David E. Williams; Daniel J. Leonard; Patrick J. Smith
The international Space Station (ISS) loses cabin atmosphere mass at some rate. Due to oxygen partial pressures fluctuations from metabolic usage, the total pressure is not a good data source for tracking total pressure loss. Using the nitrogen partial pressure is a good data source to determine the total on-orbit cabin atmosphere loss from the ISS, due to no nitrogen addition or losses. There are several important reasons to know the daily average cabin air loss of the ISS including logistics planning for nitrogen and oxygen. The total average daily cabin atmosphere loss was estimated from January 14 to April 9 of 2003. The total average daily cabin atmosphere loss includes structural leakages, Vozdukh losses, Carbon Dioxide Removal Assembly (CDRA) losses, and other component losses. The total average daily cabin atmosphere loss does not include mass lost during Extra-Vehicular Activities (EVAs), Progress dockings, Space Shuttle dockings, calibrations, or other specific one-time events.
international conference on evolvable systems | 2004
David E. Williams; Daniel J. Leonard; Valori J. Booth; Matt Russell
The International Space Station (ISS) Airlock Crewlock can be depressurized via various methods. The ISS Airlock is divided into two major sections, the Equipment Lock and Crewlock. The Equipment Lock, as the name indicates, contains the equipment to support EVA activities including Extravehicular Maneuvering/Mobility Unit (EMU) maintenance and refurbishment. The Equipment Lock also contains basic life support equipment in order to support denitrogenzation protocols while the Airlock is isolated from the rest of the ISS. The Crewlock is the section of the Airlock that is depressurized to allow for Extravehicular Activity (EVA) crewmembers to exit the ISS for performance of EVAs. As opposed to the Equipment Lock, the Crewlock is quite simple and basically just contains lights and an assembly to provide services, oxygen, coolant, etc, to the EMUs. For operational flexibility, various methods were derived for Crewlock depressurization. Herein these various different methods of ISS Airlock Crewlock depressurization will be described including their performance, impacts, and risks associated with each method. Each of the different methods will be discussed with flight data, if it exists. Models will be applied to flight cases and to other methods that have not been used on-orbit at this time.
international conference on evolvable systems | 2005
Elias Gonzalez; Daniel J. Leonard
Archive | 2011
Daniel J. Leonard; Anthony J. Cook; Daniel Lehman
Archive | 2011
Ryan N. Schaezler; Ahmed Ghariani; Daniel J. Leonard; Daniel Lehman
international conference on evolvable systems | 2007
Anthony J. Cook; Daniel J. Leonard; Patricia O'Donnell
international conference on evolvable systems | 2006
Daniel J. Leonard; Richard G. Ehmer
international conference on evolvable systems | 2005
Daniel J. Leonard
international conference on evolvable systems | 2005
Ryan N. Schaezler; Daniel J. Leonard; Saniel Suri