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).

 


Publications resulting from prior classes

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)

 


Lecture Topics (Schedule - subject to minor changes)

 

Spacecraft Life Support Systems

            Course Overview and Historical Perspectives

            Life Support Requirements Drivers and Habitability Factorsi.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)

            Water Management

            Food Supply

            Waste Processing

 

            Exam 2 (Take Home)

 

            Current Events: NASA’s Human Exploration Program

            Thanksgiving Break

 

Systems Engineering and Mission Architecture

            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:

 

Individual Effort – 60%

            40%     2 Exams (20% each)

            10%     Oral Presentation (individual effectiveness)

            10%     “Level of Effort” (peer / instructor assessment)

 

Group Effort – 40%

            15%     Group Homework / Project Status Briefings

            5%       Oral Presentation (overall effectiveness)

            20%     Final Report

 

Additional Syllabus Notes