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AAE450 Senior Spacecraft Design Kate Mitchell - 1 Kate Mitchell Week 8*: March 1 st, 2007 Human Factors – Group Lead HAB & TV Vehicle Groups This Week:

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Presentation on theme: "AAE450 Senior Spacecraft Design Kate Mitchell - 1 Kate Mitchell Week 8*: March 1 st, 2007 Human Factors – Group Lead HAB & TV Vehicle Groups This Week:"— Presentation transcript:

1 AAE450 Senior Spacecraft Design Kate Mitchell - 1 Kate Mitchell Week 8*: March 1 st, 2007 Human Factors – Group Lead HAB & TV Vehicle Groups This Week: TV and HAB Crew Cab Totals, TV Total IMLEO & IVLEO *Presented during Week 7

2 AAE450 Senior Spacecraft Design Kate Mitchell - 2 New Totals for TV & HAB Totals for each HAB Crew Cab Totals for each TV Crew Cab TV Crew Cab [Fox]HAB Crew Cab [Fox] Totals for each TV Re-supply (x5) *Total masses for HAB and TV include all human needs (structure not included).

3 AAE450 Senior Spacecraft Design Kate Mitchell - 3 TV: IMLEO & IVLEO TV 1 TV 4 TV 3 TV 2 TV Total IMLEO & IVLEO TV values include the following:  Crew Cab  Truss  Power System  Comm. System  Thermal Control System  D&C System (for spin-up)

4 AAE450 Senior Spacecraft Design Kate Mitchell - 4 Back-up Slides

5 AAE450 Senior Spacecraft Design Kate Mitchell - 5 Totals Breakdown HAB Crew Cab TV Crew Cab

6 AAE450 Senior Spacecraft Design Kate Mitchell - 6 Totals Breakdown *Volume of the Human Factors Systems is encompassed by the structures volume **Total values for the propulsion systems can be found in the files for the dE, aM, dM, aE and EP data-sharing pages ***Calculations for the total mass of each transfer vehicle for each mission are attached Example of TV Total Mass Calculation – TV 1***

7 AAE450 Senior Spacecraft Design Kate Mitchell - 7 Spacesuit Comparison Full Gas Pressure Suits Advantages –Proven technology –Various designs/sizes Disadvantages –Heavy and bulky –Difficult to donn/doff –Pre-breathe necessary –Full suit pressurization –Lack of mobility, flexibility, dexterity –Loss of oxygen if suit is damaged –High metabolic requirement MCP Suits (“Bio-Suit”) [3] Advantages –Lightweight –Minimal metabolic cost –Improved mobility, flexibility, dexterity Disadvantages –Untested technology –Difficult to donn/doff –Areas of concavity

8 AAE450 Senior Spacecraft Design Kate Mitchell - 8 Spacesuit Design Chosen Mechanical Counter Pressure Suits (“Bio-Suit”) –Overall, the Bio-Suit was found to be a better suit for exploration *Photos taken from “EVA Research at MVL” website [3]

9 AAE450 Senior Spacecraft Design Kate Mitchell - 9 References [1] Hanford, Anthony J., ed. NASA Johnson Space Center. Advanced Life Support Baseline Values and Assumptions Document. Aug. 2004. http://ston.jsc.nasa.gov/collections/TRS/_techrep/CR-2004- 208941.pdf [2] Landau, Dr. Damon F., “Strategies for the Sustained Human Exploration of Mars.” Thesis Submitted to the Faculty of Purdue University, Dec. 2006. [3] Newman, Dava. Extravehicular Activity Research at MIT Man Vehicle Laboratory: Bio-Suit Overview, 2005. http://mvl.mit.edu/EVA/biosuit/index.html [4] Reed, Ronald D., and Gary R. Coulter. "Physiology of Spaceflight." Human Spaceflight: Mission Analysis and Design. Ed. Wiley J. Larson and Linda K. Prank. New York: McGraw-Hill, 1999. 113-115. [5] Stilwell, Don, Ramzy Boutros, and Janis H. Connolly. "Crew Accommodations." Human Spaceflight: Mission Analysis and Design. Ed. Wiley J. Larson and Linda K. Prank. New York: McGraw-Hill, 1999. 575-606.


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