| PRE > " Module.........................................Descent Module Crew Size...................................................3 Length..................................................2.2 m Basic Diameter..........................................2.2 m Max Diameter............................................2.2 m Habitable Volume......................................4.00 m3 Overall Mass.........................................2,800 kg Propellants.............................................45 kg RCS Coarse Backup No x Thrust.......................6 X 10kgf RCS Propellants..........................................H2O2 Module.........................................Orbital Module Length..................................................3.4 m Basic Diameter..........................................2.3 m Max Diameter............................................2.3 m Habitable Volume......................................5.00 m3 Overall Mass.........................................1,100 kg Module.........................................Service Module Length..................................................2.3 m Basic Diameter..........................................2.1 m Max Diameter............................................2.7 m Overall Mass.........................................2,890 kg Propellants............................................500 kg RCS Coarse No x Thrust.............................14 X 10kgf RCS Fine No x Thrust................................4 X 10kgf RCS Coarse Backup No x Thrust........................8 X 1kgf RCS Fine Backup No x Thrust.....................4 X 1kgf roll RCS Propellants..........................................H2O2 Maneuver System Thrust................................417 kgf Backup Maneuver System Thrust.........................411 kgf Maneuver System Propellants.............Nitric Acid/Hydrazine Maneuver System Isp...................................282 sec Electric system...............................0.50 average kW Electric system type......Solar panel span: 9.80 m, area: 14. |
Module.........................................Descent Module Crew Size...................................................3 Length..................................................2.2 m Basic Diameter..........................................2.2 m Max Diameter............................................2.2 m Habitable Volume......................................4.00 m3 Overall Mass.........................................2,800 kg Propellants.............................................45 kg RCS Coarse Backup No x Thrust.......................6 X 10kgf RCS Propellants..........................................H2O2 Module.........................................Orbital Module Length..................................................3.4 m Basic Diameter..........................................2.3 m Max Diameter............................................2.3 m Habitable Volume......................................5.00 m3 Overall Mass.........................................1,100 kg Module.........................................Service Module Length..................................................2.3 m Basic Diameter..........................................2.1 m Max Diameter............................................2.7 m Overall Mass.........................................2,890 kg Propellants............................................500 kg RCS Coarse No x Thrust.............................14 X 10kgf RCS Fine No x Thrust................................4 X 10kgf RCS Coarse Backup No x Thrust........................8 X 1kgf RCS Fine Backup No x Thrust.....................4 X 1kgf roll RCS Propellants..........................................H2O2 Maneuver System Thrust................................417 kgf Backup Maneuver System Thrust.........................411 kgf Maneuver System Propellants.............Nitric Acid/Hydrazine Maneuver System Isp...................................282 sec Electric system...............................0.50 average kW Electric system type......Solar panel span: 9.80 m, area: 14. |
Module.........................................Descent Module Crew Size...................................................3 Length..................................................2.2 m Basic Diameter..........................................2.2 m Max Diameter............................................2.2 m Habitable Volume......................................4.00 m3 Overall Mass.........................................2,800 kg Propellants.............................................45 kg RCS Coarse Backup No x Thrust.......................6 X 10kgf RCS Propellants..........................................H2O2 |
Module.........................................Descent Module Crew Size...................................................3 Length..................................................2.2 m Basic Diameter..........................................2.2 m Max Diameter............................................2.2 m Habitable Volume......................................4.00 m3 Overall Mass.........................................2,800 kg Propellants.............................................45 kg RCS Coarse Backup No x Thrust.......................6 X 10kgf RCS Propellants..........................................H2O2 |
Module.........................................Descent Module Crew Size...................................................3 Length..................................................2.2 m Basic Diameter..........................................2.2 m Max Diameter............................................2.2 m Habitable Volume......................................4.00 m3 Overall Mass.........................................2,800 kg Propellants.............................................45 kg RCS Coarse Backup No x Thrust.......................6 X 10kgf RCS Propellants..........................................H2O2 |