ESA Document - Emits - ESA
ESA Document - Emits - ESA ESA Document - Emits - ESA
s Degree of Recycling (%) OXYGEN 95 POTABLE WATER 95 GREY WATER (condensate, used hygiene water) 95 YELLOW WATER (water in contact with urine) 95 BLACK WATER (water in contact with Faeces) 20 SOLID ORGANIC WASTE TO FOOD 20 SOLID INORGANIC WASTE 0 PACKAGING REUSE 0 Table 3-15: Anticipated degrees of recycling HMM Assessment Study Report: CDF-20(A) February 2004 page 164 of 422 The system mass has been estimated to be 13.4 tonnes. The savings on the LSS mass must be evaluated carefully due to the large uncertainty on the state of the development of certain subsystems. However, the impact on the consumables is significant as shown in Table 3-16. CONSUMABLES TO BE LAUNCHED (kg) OXYGEN 394.2 NITROGEN 91.0 POTABLE WATER 1008.8 HYGIENE WATER 323.6 DRY FOOD 3830.9 PACKAGING 1392.3 INORGANIC MATERIAL ECXLUDING PACKAGING 3177.9 TOTAL 10218.6 WASTE PRODUCTION DURING MISSION (kg) WASTE GASES 306.5 WASTE WATER 1000.8 SOLID ORGANIC WASTE 804.9 SOLID INORGANIC WASTE EXCLUDING PACKAGING 3177.9 PACKAGING 1392.3 TOTAL 6682.4 ROUGH ESTIMATE ECLSS MASS (kg) TOTAL 13627.6 Table 3-16: Mass estimates for a mission using anticipated technology Due to the anticipated high-recycling efficiencies the amount of needed consumables is reduced to 10.3 tonnes. In addition, the amount of produced waste is reduced to 6.7 tonnes making alternative options to jettison more likely. The life support system has been estimated to have an approximate mass of 13.4 tonnes. The detailed mass budget is shown in Table 3-17. Equipment Number Mass per of units unit (kg) ALS Airlock Air Save Pump Package 2.00 70.30 ALS ARSD CDRA (ARES DEMONSTRATOR) 3.00 202.00 ALS CONVENTIONAL OVEN 2.00 50.00 ALS COOKING/EATING SUPPLY 2.00 5.00 ALS HAND/MOUNTH WASH FAUCET 2.00 8.00 ALS METOX CO2 removal (canister) 3.00 14.52 ALS METOX CO2 removal (regenerator) 1.00 47.63 ALS SHOWER 2.00 75.00
s HMM Assessment Study Report: CDF-20(A) February 2004 page 165 of 422 Equipment Number Mass per of units unit (kg) ALS VACUUM 3.00 30.00 GENERIC ACCUMULATOR HYGIENE WATER (300L) 4.00 100.00 GENERIC ACCUMULATOR POTABLE WATER (300L) 2.00 100.00 GENERIC ACCUMULATOR URINE STORAGE TANK (57L) 1.00 30.84 GENERIC INORGANIC STORAGE(200kg) 16.00 67.00 GENERIC ORGANIC STORAGE(200kg) 20.00 80.00 ISS AAA - avionics air assembly 10.00 12.40 ISS ACCUMULATOR WASTE WATER TANK (46L) 1.00 67.59 ISS CCAA 2.00 112.00 ISS comode/urinal 3.00 50.00 ISS condensate storage 1.00 21.20 ISS EMU (Shuttle) 7.00 135.00 ALS FREEZER 1.00 400.00 ISS fuel cell water storage 4.00 21.20 ISS HEPA - BACTERIAL FILTER 40.00 5.20 ISS IMV - intermodule ventilation fan assembly 20.00 4.76 ISS IMV - intermodule ventilation valve 4.00 5.10 ISS laundry (washer/dryer) 2.00 118.00 ISS OXYGEN STORAGE TANK 5.00 109.00 ISS OXYGEN TANK PRESSURISATION SYSTEM 2.00 102.00 ISS PCWQM - process control water quality monitoring 2.00 38.00 ISS PFE - portable fire extinguisher 5.00 15.10 ISS Sample Delivery System 4.00 2.70 ISS smoke detector 10.00 1.50 ISS TCCS - trace contaminant control system 2.00 78.20 ISS trash compactor 2.00 27.00 ISS URINE PROCESSOR ASSEMBLY (VCD) 2.00 245.00 ALS BWRS1 (316l vessel) 3.00 332.80 Manual Pressure Equalization Valve (MPEV) 4.00 1.20 microwave oven 2.00 70.00 sink and spigot 2.00 15.00 GENERIC PERSONAL STOWAGE SPACE (50kg) 6.00 50.00 RESTRAINTS AND MOBILITY AIDS (100kg) 2.00 100.00 GENERIC TOOLS EQUIPMENT (20kg) 50.00 20.00 GENERIC MEDICAL/SURGICAL/DENTAL SUITE (1000kg for Mars Mission) 1.00 1000.00 SLEEP PROVISIONS 6.00 9.00 GENERIC OPERATIONAL SUPPLIES (20kg) 6.00 20.00 personal hygiene kit 18.00 1.80 Portable Breathing Aparatus 12.00 1.20 Pressure Control Assembly (PCA) 4.00 78.20 X-38 HI PRESSURE G02 REGULATOR 2.00 1.40 X-38 HI PRESSURE GN2 REGULATOR 2.00 1.40 X-38 LOW PRESSURE G02 REGULATOR 2.00 1.40 X-38 LOW PRESSURE GN2 REGULATOR 2.00 1.76 ISS NITROGEN STORAGE TANK 1.00 109.00 GENERIC CLOTHING 10kg 9.00 10.00 ALS Lyophilizer 2.00 250.00 ALS Lyophilizer 2.00 250.00 Table 3-17: Detailed mass budget for the anticipated life support system
- Page 113 and 114: s 2.10.2.2.2 LEO assembly HMM Asses
- Page 115 and 116: s HMM Assessment Study Report: CDF-
- Page 117 and 118: s Basic RF link Four 70-m Ka-band s
- Page 119 and 120: s HMM Assessment Study Report: CDF-
- Page 121 and 122: s HMM Assessment Study Report: CDF-
- Page 123 and 124: s HMM Assessment Study Report: CDF-
- Page 125 and 126: s 3 TRANSFER VEHICLE 3.1 Systems…
- Page 127 and 128: s Operational Requirements It shall
- Page 129 and 130: s Trans Mars Injection Module Mars
- Page 131 and 132: s Figure 3-2: Parallel configuratio
- Page 133 and 134: s Figure 3-6: Global dimensions com
- Page 135 and 136: s Front Node 3.2.3.1.3 EVA systems
- Page 137 and 138: s Trans Mars Injection (three stage
- Page 139 and 140: s Figure 3-16: Recommendations for
- Page 141 and 142: s Factors to be considered Impacts
- Page 143 and 144: s HMM Assessment Study Report: CDF-
- Page 145 and 146: s HMM Assessment Study Report: CDF-
- Page 147 and 148: s HMM Assessment Study Report: CDF-
- Page 149 and 150: s Figure 3-24: Baseline design back
- Page 151 and 152: s Figure 3-26: Baseline design priv
- Page 153 and 154: s Module part 3............= 0 m 3
- Page 155 and 156: s 3.3.2.1 Requirements and design d
- Page 157 and 158: s HMM Assessment Study Report: CDF-
- Page 159 and 160: s HMM Assessment Study Report: CDF-
- Page 161 and 162: s HMM Assessment Study Report: CDF-
- Page 163: s HMM Assessment Study Report: CDF-
- Page 167 and 168: s 3.3.3.1 Requirements and design d
- Page 169 and 170: s HMM Assessment Study Report: CDF-
- Page 171 and 172: s HMM Assessment Study Report: CDF-
- Page 173 and 174: s HMM Assessment Study Report: CDF-
- Page 175 and 176: s HMM Assessment Study Report: CDF-
- Page 177 and 178: s flux [W/m2] 250 200 150 100 50 0
- Page 179 and 180: s Figure 3-38: Power required to ma
- Page 181 and 182: s HMM Assessment Study Report: CDF-
- Page 183 and 184: s HMM Assessment Study Report: CDF-
- Page 185 and 186: s 3.3.4.3 Assumptions and trade-off
- Page 187 and 188: s 3.3.4.3.3 Power conditioning and
- Page 189 and 190: s 3.3.5 AOCS HMM Assessment Study R
- Page 191 and 192: s HMM Assessment Study Report: CDF-
- Page 193 and 194: s Configuration Length (m) Total ma
- Page 195 and 196: s 3.3.5.5 ACS for TMI 1 st HMM Asse
- Page 197 and 198: s HMM Assessment Study Report: CDF-
- Page 199 and 200: s HMM Assessment Study Report: CDF-
- Page 201 and 202: s HMM Assessment Study Report: CDF-
- Page 203 and 204: s HMM Assessment Study Report: CDF-
- Page 205 and 206: s 3.3.6.2 Baseline design HMM Asses
- Page 207 and 208: s HMM Assessment Study Report: CDF-
- Page 209 and 210: s 5 Reduce 2dB pointing precision t
- Page 211 and 212: s 70-m antenna 70-m antenna 3.3.7.5
- Page 213 and 214: s Angular separation SEM > 10º SEM
s<br />
HMM<br />
Assessment Study<br />
Report: CDF-20(A)<br />
February 2004<br />
page 165 of 422<br />
Equipment Number Mass per<br />
of units unit (kg)<br />
ALS VACUUM 3.00 30.00<br />
GENERIC ACCUMULATOR HYGIENE WATER (300L) 4.00 100.00<br />
GENERIC ACCUMULATOR POTABLE WATER (300L) 2.00 100.00<br />
GENERIC ACCUMULATOR URINE STORAGE TANK (57L) 1.00 30.84<br />
GENERIC INORGANIC STORAGE(200kg) 16.00 67.00<br />
GENERIC ORGANIC STORAGE(200kg) 20.00 80.00<br />
ISS AAA - avionics air assembly 10.00 12.40<br />
ISS ACCUMULATOR WASTE WATER TANK (46L) 1.00 67.59<br />
ISS CCAA 2.00 112.00<br />
ISS comode/urinal 3.00 50.00<br />
ISS condensate storage 1.00 21.20<br />
ISS EMU (Shuttle) 7.00 135.00<br />
ALS FREEZER 1.00 400.00<br />
ISS fuel cell water storage 4.00 21.20<br />
ISS HEPA - BACTERIAL FILTER 40.00 5.20<br />
ISS IMV - intermodule ventilation fan assembly 20.00 4.76<br />
ISS IMV - intermodule ventilation valve 4.00 5.10<br />
ISS laundry (washer/dryer) 2.00 118.00<br />
ISS OXYGEN STORAGE TANK 5.00 109.00<br />
ISS OXYGEN TANK PRESSURISATION SYSTEM 2.00 102.00<br />
ISS PCWQM - process control water quality monitoring 2.00 38.00<br />
ISS PFE - portable fire extinguisher 5.00 15.10<br />
ISS Sample Delivery System 4.00 2.70<br />
ISS smoke detector 10.00 1.50<br />
ISS TCCS - trace contaminant control system 2.00 78.20<br />
ISS trash compactor 2.00 27.00<br />
ISS URINE PROCESSOR ASSEMBLY (VCD) 2.00 245.00<br />
ALS BWRS1 (316l vessel) 3.00 332.80<br />
Manual Pressure Equalization Valve (MPEV) 4.00 1.20<br />
microwave oven 2.00 70.00<br />
sink and spigot 2.00 15.00<br />
GENERIC PERSONAL STOWAGE SPACE (50kg) 6.00 50.00<br />
RESTRAINTS AND MOBILITY AIDS (100kg) 2.00 100.00<br />
GENERIC TOOLS EQUIPMENT (20kg) 50.00 20.00<br />
GENERIC MEDICAL/SURGICAL/DENTAL SUITE (1000kg for Mars Mission) 1.00 1000.00<br />
SLEEP PROVISIONS 6.00 9.00<br />
GENERIC OPERATIONAL SUPPLIES (20kg) 6.00 20.00<br />
personal hygiene kit 18.00 1.80<br />
Portable Breathing Aparatus 12.00 1.20<br />
Pressure Control Assembly (PCA) 4.00 78.20<br />
X-38 HI PRESSURE G02 REGULATOR 2.00 1.40<br />
X-38 HI PRESSURE GN2 REGULATOR 2.00 1.40<br />
X-38 LOW PRESSURE G02 REGULATOR 2.00 1.40<br />
X-38 LOW PRESSURE GN2 REGULATOR 2.00 1.76<br />
ISS NITROGEN STORAGE TANK 1.00 109.00<br />
GENERIC CLOTHING 10kg 9.00 10.00<br />
ALS Lyophilizer 2.00 250.00<br />
ALS Lyophilizer 2.00 250.00<br />
Table 3-17: Detailed mass budget for the anticipated life support system
Change language