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10,000 PEOPLE IN SPACE-SANITARY ENGINEERING IN THE YEAR 2000 Harold J. Jebens, Associate Professor Department of Civil Engineering University of Wisconsin-Platteville Platteville, Wisconsin 53818 INTRODUCTION Establishing permanent human communities in space has often been proposed by science fiction authors [1-4]. Recently, however, serious proposals for constructing large rotating space colonies with an earth-like interior have been presented [5] and have attracted considerable attention [6-9]. The National Aeronautics and Space Administration (NASA) has indicated interest in such a colony and during the summer of 1975 hosted a group of nineteen faculty members, six students and three volunteers to perform a system design study on space colonization [10]. Cosponsors of the project with NASA were Stanford University and the American Society for Engineering Education. This paper describes the life support system selected for the baseline design of the colony. The objective of the summer study was to design a space colony for permanent habitation by 10,000 people that would be physiologically safe, socially viable and economically justified while being accomplished with near-term technology. The colony would be constructed in space orbiting around L-5, a point in lunar orbit equidistant from the earth and the moon that follows the moon as it revolves around the earth. Raw materials from the moon would be transported to the colony site, refined and fabricated into the toroidal-shaped habitat shown in schematic in Figure 1. Physiological and aesthetic constraints necessary for permanent human occupancy dictated the shape of the habitat and its earth-like interior (Figure 2), thereby precluding the use of rotating cylinders as proposed in Physics Today [5]. The inhabitants of the colony would construct and service large (>5000 Mw) solar power stations utilizing photovoltaic [11] or thermal methods [12] of solar conversion. The power stations would collect solar energy and transmit the energy to earth via microwaves, thereby producing sufficient revenue to justify the expense of constructing the colony. LIFE SUPPORT REQUIREMENTS The life support system of the colony must meet the inhabitants' metabolic requirements for food, water and oxygen while removing their solid, liquid and gaseous waste. Table I lists the quantities of materials required and produced by an individual astronaut [13], a space shuttle crew member [14] and a space colonist. Minor differences in the table reflect the difference in size of the average individual supported by each system. Women crew members will be in the shuttle and children will be present in the space colony. The difference in food and water requirements are indicative of the type of food supplied-the astronauts and shuttle personnel dine on condensed or dehydrated foods and thus must consume higher quantities of water; the space colonist enjoys an earth-like diet where fruit juice is counted as food rather than as solids and reconstituting water. To date, life support systems for space vehicles have been completely open systems. Supplies for metabolic requirements were either stored expendables or resupplied from earth or vented to space. Failure to provide regeneration systems in space vehicles has been due to the relatively short mission durations in past and scheduled missions. As missions have lengthened, the components needed for a life support system also increased in complexity [15,16]. Figure 3 indicates the effect of mission duration on the weight of the system for various degrees of life support loop closure. As evident in the figure, the closure of a subsystem (water, atmosphere or food) causes an increased initial weight 668
Object Description
Purdue Identification Number | ETRIWC197660 |
Title | 10,000 people in space : sanitary engineering in the year 2000 |
Author | Jebens, Harold J. |
Date of Original | 1976 |
Conference Title | Proceedings of the 31st Industrial Waste Conference |
Conference Front Matter (copy and paste) | http://e-archives.lib.purdue.edu/u?/engext,27048 |
Extent of Original | p. 668-675 |
Collection Title | Engineering Technical Reports Collection, Purdue University |
Repository | Purdue University Libraries |
Rights Statement | Digital object copyright Purdue University. All rights reserved. |
Language | eng |
Type (DCMI) | text |
Format | JP2 |
Date Digitized | 2009-07-08 |
Capture Device | Fujitsu fi-5650C |
Capture Details | ScandAll 21 |
Resolution | 300 ppi |
Color Depth | 8 bit |
Description
Title | page 668 |
Collection Title | Engineering Technical Reports Collection, Purdue University |
Repository | Purdue University Libraries |
Rights Statement | Digital object copyright Purdue University. All rights reserved. |
Language | eng |
Type (DCMI) | text |
Format | JP2 |
Capture Device | Fujitsu fi-5650C |
Capture Details | ScandAll 21 |
Transcript | 10,000 PEOPLE IN SPACE-SANITARY ENGINEERING IN THE YEAR 2000 Harold J. Jebens, Associate Professor Department of Civil Engineering University of Wisconsin-Platteville Platteville, Wisconsin 53818 INTRODUCTION Establishing permanent human communities in space has often been proposed by science fiction authors [1-4]. Recently, however, serious proposals for constructing large rotating space colonies with an earth-like interior have been presented [5] and have attracted considerable attention [6-9]. The National Aeronautics and Space Administration (NASA) has indicated interest in such a colony and during the summer of 1975 hosted a group of nineteen faculty members, six students and three volunteers to perform a system design study on space colonization [10]. Cosponsors of the project with NASA were Stanford University and the American Society for Engineering Education. This paper describes the life support system selected for the baseline design of the colony. The objective of the summer study was to design a space colony for permanent habitation by 10,000 people that would be physiologically safe, socially viable and economically justified while being accomplished with near-term technology. The colony would be constructed in space orbiting around L-5, a point in lunar orbit equidistant from the earth and the moon that follows the moon as it revolves around the earth. Raw materials from the moon would be transported to the colony site, refined and fabricated into the toroidal-shaped habitat shown in schematic in Figure 1. Physiological and aesthetic constraints necessary for permanent human occupancy dictated the shape of the habitat and its earth-like interior (Figure 2), thereby precluding the use of rotating cylinders as proposed in Physics Today [5]. The inhabitants of the colony would construct and service large (>5000 Mw) solar power stations utilizing photovoltaic [11] or thermal methods [12] of solar conversion. The power stations would collect solar energy and transmit the energy to earth via microwaves, thereby producing sufficient revenue to justify the expense of constructing the colony. LIFE SUPPORT REQUIREMENTS The life support system of the colony must meet the inhabitants' metabolic requirements for food, water and oxygen while removing their solid, liquid and gaseous waste. Table I lists the quantities of materials required and produced by an individual astronaut [13], a space shuttle crew member [14] and a space colonist. Minor differences in the table reflect the difference in size of the average individual supported by each system. Women crew members will be in the shuttle and children will be present in the space colony. The difference in food and water requirements are indicative of the type of food supplied-the astronauts and shuttle personnel dine on condensed or dehydrated foods and thus must consume higher quantities of water; the space colonist enjoys an earth-like diet where fruit juice is counted as food rather than as solids and reconstituting water. To date, life support systems for space vehicles have been completely open systems. Supplies for metabolic requirements were either stored expendables or resupplied from earth or vented to space. Failure to provide regeneration systems in space vehicles has been due to the relatively short mission durations in past and scheduled missions. As missions have lengthened, the components needed for a life support system also increased in complexity [15,16]. Figure 3 indicates the effect of mission duration on the weight of the system for various degrees of life support loop closure. As evident in the figure, the closure of a subsystem (water, atmosphere or food) causes an increased initial weight 668 |
Resolution | 300 ppi |
Color Depth | 8 bit |
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