ESA Document - Emits - ESA
ESA Document - Emits - ESA ESA Document - Emits - ESA
s • Easy ground reference and testing possible • Long-term exposure to other atmospheres has not been studied thoroughly HMM Assessment Study Report: CDF-20(A) February 2004 page 158 of 422 Preferably, the atmosphere would be free of any contaminants. However, as a minimum requirement, the spacecraft atmosphere shall adhere to the requirements given in ESA PSS-03- 401. Based on the experiences with long-term pressurised spacecrafts there shall be more stringent limits on microbial contamination. The following limit has been proposed during this study based on the recommendation by ESA internal experts: Total microflora count: 200 CFU/m 3 (CFU stands for colony forming units) 3.3.2.2.4 Waste production Besides the already presented production of faecal material by the crew, the crew will produce additional organic and inorganic waste. Organic waste will consist of hair, nail clippings, skin material, kitchen waste, food leftovers. The total amount of such organic waste has been estimated to be 0.1 kg/crew/day. To quantify the total amount of inorganic waste produced by the crew per day was not possible due to the lack of data. However, reviewing existing data and other sizing tools, the amount of inorganic waste produced by the crew per day was estimated to be around 0.6 kg/crew/day. This includes: 0.05 kg/d cleaning supplies 0.1 kg/d waste collection supplies 0.1 kg/d contingency collection mitten bags 0.1 kg/d hygiene supplies 0.2 kg/d wet wipes for house cleaning 3.3.2.2.5 Packaging A significant fraction of the inorganic waste will come from the food packaging. Packaging of food has been investigated to establish a figure that could be used during the study. The work included a paper review and a small weighing exercise to verify the numbers. The review revealed differences in the food packaging between the food provided by the Russian and the American organisations. While the Russians use many cans for packaging their foods, most of the thermostabilized entrees offered by the U.S. are packaged in retort pouches. The U.S. discontinued the use of space food in tubes in the early 1970s. Russia has used tubes continually, but is now beginning to phase them out. Preservation methods for Russian food is comparable to that of Shuttle food but different materials and packages are used. Preservation methods consist mostly of dehydration, thermostabilization, and intermediate moisture. Packaging includes metal tubes, cans, and plastic overwrapped in foil. Russian cans are made of steel, require a can opener, and come in two sizes: large (101.6 mm in diameter x 38.1 mm high) and small (73.025 mm in diameter x 31.75 mm high). In addition to steel cans, the Russians use a plastic packaging material for dehydrated and intermediate moisture foods. They do not have sufficient barrier properties for extended shelf life, so the
s HMM Assessment Study Report: CDF-20(A) February 2004 page 159 of 422 plastic packaging material is overwrapped with a foil material to extend the shelf life (NASA Food Technology Commercial Space Centre). Packaging on the U.S. side (considered lighter because of the use of plastics rather than cans) can be considered 220 g/(day*crew) for Shuttle missions and slightly higher for ISS due to overwrap films and the additional thermostabilized pouches. For comparison, food with relatively low humidity content was weighed and the ratio between packaging and food was established. Test articles were dry ice cream, dried roasted seaweed, mashed potato powder, instant soup and dried fungi. The average packaging to food ratio was 0.34(kgpackaging/kgfood) for ‘meal size’ ratios. Based on the dry food demand of the crew of aboout 0.674 kg/(day*crew) and the data obtained from NASA, the current packaging to food ratio is about 0.33(kgpackaging/kgfood) and for ISS slightly higher. Based on this outcome, the study considered 270 gpackaging/(day*crew) based on 0.674 kg dry food per day and crew and a packing ratio of 0.4). Although this seems high, for a long duration mission some food will probably be produced in-situ and needs additional packaging as well as the more stringent demands on the food preservation. 3.3.2.2.6 EVA considerations Based on the uncertainties regarding the conditions of crew as well as the environment during trans-planetary flight, the frequency of EVA needs to be kept to a minimum. However, provisions for emergency EVAs need to be foreseen to be able to recover to more favorable spacecraft performance. Therefore the capability of performing EVAs during transit has been implemented. 3.3.2.2.7 Contingency supply Using a regenerative system it would be sufficient to launch the initial filling of the systems and the make-up supply depending on the recycling efficiencies. However, it is necessary to provide the crew with contingency supply if the life support system is failing. In an ideal case the contingency supply would enable the crew to safely return to Earth. Apart from that, as a result of the abort analysis it was discovered that no extra contingency is required in the ECLSS system to cope with these scenarios: Emergency supply of oxygen: 36 days Emergency supply of potable water: 10 days Emergency supply of hygiene water: 5 days Emergency supply of food: 10 days Currently, the assumption is that the supply would be sufficient for the crew to overcome the contingency situation or to determine an alternative consumables supply strategy. It is clear that these figures may significantly change but they give a reasonable starting point for further discussions. In addition, this contingency supply shall be accessible from the radiation shelter as the supply for an eventual stay inside. 3.3.2.2.8 Food production unit (Greenhouse)
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s<br />
HMM<br />
Assessment Study<br />
Report: CDF-20(A)<br />
February 2004<br />
page 159 of 422<br />
plastic packaging material is overwrapped with a foil material to extend the shelf life (NASA<br />
Food Technology Commercial Space Centre).<br />
Packaging on the U.S. side (considered lighter because of the use of plastics rather than cans)<br />
can be considered 220 g/(day*crew) for Shuttle missions and slightly higher for ISS due to<br />
overwrap films and the additional thermostabilized pouches.<br />
For comparison, food with relatively low humidity content was weighed and the ratio between<br />
packaging and food was established. Test articles were dry ice cream, dried roasted seaweed,<br />
mashed potato powder, instant soup and dried fungi. The average packaging to food ratio was<br />
0.34(kgpackaging/kgfood) for ‘meal size’ ratios.<br />
Based on the dry food demand of the crew of aboout 0.674 kg/(day*crew) and the data obtained<br />
from NASA, the current packaging to food ratio is about 0.33(kgpackaging/kgfood) and for ISS<br />
slightly higher.<br />
Based on this outcome, the study considered 270 gpackaging/(day*crew) based on 0.674 kg dry<br />
food per day and crew and a packing ratio of 0.4). Although this seems high, for a long duration<br />
mission some food will probably be produced in-situ and needs additional packaging as well as<br />
the more stringent demands on the food preservation.<br />
3.3.2.2.6 EVA considerations<br />
Based on the uncertainties regarding the conditions of crew as well as the environment during<br />
trans-planetary flight, the frequency of EVA needs to be kept to a minimum. However,<br />
provisions for emergency EVAs need to be foreseen to be able to recover to more favorable<br />
spacecraft performance. Therefore the capability of performing EVAs during transit has been<br />
implemented.<br />
3.3.2.2.7 Contingency supply<br />
Using a regenerative system it would be sufficient to launch the initial filling of the systems and<br />
the make-up supply depending on the recycling efficiencies. However, it is necessary to provide<br />
the crew with contingency supply if the life support system is failing. In an ideal case the<br />
contingency supply would enable the crew to safely return to Earth. Apart from that, as a result<br />
of the abort analysis it was discovered that no extra contingency is required in the ECLSS system<br />
to cope with these scenarios:<br />
Emergency supply of oxygen: 36 days<br />
Emergency supply of potable water: 10 days<br />
Emergency supply of hygiene water: 5 days<br />
Emergency supply of food: 10 days<br />
Currently, the assumption is that the supply would be sufficient for the crew to overcome the<br />
contingency situation or to determine an alternative consumables supply strategy. It is clear that<br />
these figures may significantly change but they give a reasonable starting point for further<br />
discussions. In addition, this contingency supply shall be accessible from the radiation shelter as<br />
the supply for an eventual stay inside.<br />
3.3.2.2.8 Food production unit (Greenhouse)