AIR1168/14 Spacecraft Life Support Systems

Reaffirmed

06/20/2011

Features
Issuing Committee
Scope
Content
A life support system (LSS) is usually defined as a system that provides elements necessary for maintaining human life and health in the state required for performing a prescribed mission. The LSS, depending upon specific design requirements, will provide pressure, temperature, and composition of local atmosphere, food, and water. It may or may not collect, dispose, or reprocess wastes such as carbon dioxide, water vapor, urine, and feces.
It can be seen from the preceding definition that LSS requirements may differ widely, depending on the mission specified, such as operation in Earth orbit or lunar mission. In all cases the time of operation is an important design factor. An LSS is sometimes briefly defined as a system providing atmospheric control and water, waste, and thermal management.
The major subsystems required to accomplish the general functions mentioned above are:
  1. 1
    Breathing and pressurization gas storage system.
  2. 2
    Temperature and humidity control system.
  3. 3
    Carbon dioxide control system.
  4. 4
    Trace contaminant control system.
  5. 5
    Water management system.
  6. 6
    Waste management system.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR1168/14
Pages
98
Citation
SAE International Information Report, Spacecraft Life Support Systems, SAE Standard AIR1168/14, Reaffirmed June 2011, Issued January 1995, https://doi.org/10.4271/AIR1168/14.
Additional Details
Publisher
Published
Jun 20, 2011
Product Code
AIR1168/14
Content Type
Information Report
Status
Reaffirmed
Language
English

Revisions