2001SAE technical papers on CD-ROM/SAE technical paper seriesRequires access

International Space Station (ISS) United States (US) Laboratory Module Environmental Control and Life Support (ECLS) System Close-Out Process for Launch

Gregory J. Gentry, R. P. Reysa, Gary L. Wentz

Open publisher page 0 citations

Abstract

The International Space Station (ISS) United States Laboratory module has been under test for approximately two years in the Space Station Processing Facility (SSPF) at NASA Kennedy Space Center (KSC) preparing for launch. Preparation activities for closing out the Environmental Control and Life Support (ECLS) system have included Closed Hatch testing to verify the capability of the life support equipment to support the crew, final manufacturing steps, and the close-out process itself. These activities were accomplished by an integrated Boeing and NASA team, located at the Johnson Space Center (Houston, Texas), Marshall Space Flight Center (Huntsville, Alabama) and Kennedy Space Center, Florida. On December 13, the Laboratory module hatches were sealed prior to loading into the Shuttle Orbiter payload bay for launch on February 7, 2001. This paper will address the Laboratory module ECLS hardware configuration including off-gas testing, baseline cabin sampling used to compute initial on-orbit ingress contaminant load, final purge, and cabin pressure adjustment for launch.

About this research paper

What this paper is about

The International Space Station (ISS) United States Laboratory module has been under test for approximately two years in the Space Station Processing Facility (SSPF) at NASA Kennedy Space Center (KSC) preparing for launch. Preparation activities for closing out the Environmental Control and Life Support (ECLS) system have included Closed Hatch testing to verify the capability of the life support equipment to support the crew, final manufacturing steps, and the close-out process itself. These activities were accomplished by an integrated Boeing and NASA team, located at the Johnson Space Center (Houston, Texas), Marshall Space Flight Center (Huntsville, Alabama) and Kennedy Space Center, Florida. On December 13, the Laboratory module hatches were sealed prior to loading into the Shuttle Orbiter payload bay for launch on February 7, 2001. This paper will address the Laboratory module ECLS hardware configuration including off-gas testing, baseline cabin sampling used to compute initial on-orbit ingress contaminant load, final purge, and cabin pressure adjustment for launch.

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

The International Space Station (ISS) United States Laboratory module has been under test for approximately two years in the Space Station Processing Facility (SSPF) at NASA Kennedy Space Center (KSC) preparing for launch. Preparation activities for closing out the Environmental Control and Life Support (ECLS) system have included Closed Hatch testing to verify the capability of the life support equipment to support the crew, final manufacturing steps, and the close-out process itself. These activities were accomplished by an integrated Boeing and NASA team, located at the Johnson Space Center (Houston, Texas), Marshall Space Flight Center (Huntsville, Alabama) and Kennedy Space Center, Florida. On December 13, the Laboratory module hatches were sealed prior to loading into the Shuttle Orbiter payload bay for launch on February 7, 2001. This paper will address the Laboratory module ECLS hardware configuration including off-gas testing, baseline cabin sampling used to compute initial on-orbit ingress contaminant load, final purge, and cabin pressure adjustment for launch.

Key concepts: International Space Station, Life support system, Aeronautics, Process (computing), Life support, Space (punctuation), Aerospace engineering, Systems engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
International Space Station (ISS) United States (US) Laboratory Module Environmental Control and Life Support (ECLS) System Close-Out Process for Launch — Research Paper | ScholarLens