Updated 12/18/2006 3:05 PM
Spacecraft Life Support Systems
ASEN 5116 Spring 2006
Tu/Th 0800-0915
Room ITLL 1B50
Instructor
Dr. David Klaus
office: ECAE 107
ph. (303) 492-3525
email: klaus@colorado.edu
Course Overview
Provides a working knowledge of the systems needed to sustain human life in a spacecraft environment. Emphasis on understanding functional requirements of a life support system; operational details of subsystem technologies; new concepts currently being considered in NASA's advanced programs; and conducting a technical trade study.
Text: Spaceflight Life Support and Biospherics by Peter Eckart, Space Tech. Library Vol. 5, Kluwer Academic Publishers & Microcosm Press, 1996
Course Objectives
To provide engineering students with a working knowledge of the integrated systems needed to optimally sustain human life in a spacecraft environment.
Specific subject matter includes:
- functional requirements of a spacecraft life support system
- operational details of life support technologies
- conducting technical trade studies
- new concepts currently being considered in NASA’s advanced programs
- systems integration, analysis and operations
The semester concurrently entails a series of lectures, evaluated by homework, quizzes and an exam, and a group project involving requirement definition and conceptual design of a spacecraft life support system. The project consists of group homework assignments, interim and final oral presentations, and a written final report, which previous classes (ASEN 5116 and 5158) have turned into published papers or technical reports (see list below).
Kobrick, R.L., Baca, D., Cloutier, C., Gauthier, B., Geschwill, L., Gustafson, A., O’Dell, S., and Klaus, D. (2006): “Next Generation Lunar Lander: Preliminary Mass Estimate Summary”. Technical Report submitted in response to NASA Request for Information (RFI) Lunar Lander Concept Studies (NNJ06LSAM05L) (pdf)
Klaus, D.M., Adams, A.C., Bamsey, M., Cragg, M., Ellis, T., Higgins, C.D., Howard, H.N., Jairala, J., Kelly, E.A., Krauser, W.R., McFarland, S.M. and Vellone, M.M. (2005) “Spacecraft Life Support System Design Guidelines for Human Exploration of the Moon and Mars” SAE Technical Paper ICES 2005-01-3008 (pdf)
Klaus, D., Chluda, H., Ellis, T., Fehring, J., Howard, H., Jairala, J., Lloyd, T., Matthews, D., Morris, K., Rowley, K., Sauers, C. and Stephens, T. (2004) “Systems Engineering Evaluation of a Mars Habitat Design” ICES, SAE Technical Paper ICES 2004-01-2372 (pdf)
Czupalla, M., Aponte, V., Chappell, S. and Klaus, D. (2004) “Analysis of a Spacecraft Life Support System for a Mars Mission” Acta Astronautica 55: 537-547 (pdf)
Semester Project
Reference
Klaus, D., Bamsey, M., Schuller, M.,
Godard, O., Little, F. and Askew, R. (2006) Defining space suit functional
design requirements for lunar and Mars exploration missions, SAE Technical Paper 2006-01-2290 (pdf)
Spacecraft
Life Support Systems
Course Overview and Historical Perspectives
Life Support Requirements Drivers and Habitability Factors – i.e. the human in the loop
EVA Requirements Drivers – i.e. the human in the space suit
Overview of Prior Life Support Systems
Spaceship Earth and
Extraterrestrial Environments
Fundamentals of terrestrial ecology and scaling down to spacecraft constraints
Ascent, Abort, Orbital and Descent stages and Lunar and Mars surfaces
Design Process and Fundamentals of Life Support
Functional LSS Schematic Flow Diagram
Mission Design Factors, Definitions, Requirement Hierarchy (0,1,2,3) and Phases (A,B,C/D,E)
Exam 1
Subsystem
Technologies
Physico-Chemical vs. Bioregenerative Life Support Approaches
Conducting Trade Studies – technology, subsystem and system levels
EVA - space suit design considerations
Atmosphere Management (CO2, O2, N2, TCC, THC, FDS)
Exam 2 (Take Home)
Current Events: NASA’s Human Exploration Program
Thanksgiving Break
Systems Engineering
and
Subsystem Integration and Interface Definitions
Technology Readiness Level (TRL) and Equivalent System Mass (ESM)
Modeling, Analysis, and Operational Considerations
Project Focus
Spacesuit Concepts for Lunar and Mars Exploration Missions
Grades will be derived from individual participation and the various group deliverables as follows:
40% 2 Exams (20% each)
10% Oral Presentation (individual effectiveness)
10% “Level of Effort” (peer / instructor assessment)
15% Group Homework / Project Status Briefings
5% Oral Presentation (overall effectiveness)
20% Final Report