erv - 1 end of semester presentation 12-09-03 brad buchanan – group leader dominic amaturo
TRANSCRIPT
Misson Architecture
• 2 launches using Magnum Booster
• ~ 243 day Hohmann Transfer to Mars
• 740 day stay to generate fuel/water/oxygen
• Crew arrives, stay for 550 days
• Liftoff from Mars
• ~ 243 day Hohmann Transfer return to Earth
• Return to Earth in LEO
Structures
• ~ 25 feet diameter, 80 feet long• Sepcore semi-ablative heat shield• Graphite/Magnesium metal matrix
composite• Individual bulkheads
Propulsion
• Four Pratt & Whitney RL10-series engines modified to use methane for main engines
– Isp of 376 seconds
– 155 kN of thrust per engine
– 2 meters long, 1 meter diameter, 363 kg
Ground Control
• Locations of MCC, SOCC, and POCC are to be determined next semester
• Deep Space Network
• Remote Agent System
Communications
• Optical Communication
• 1% antenna area
• Narrow Beam Divergence
Source: http://lasers.jpl.nasa.gov/
Power
• Main Power / Secondary Power
• Hydrogen fuel cells
• 4 Pu-238 RTG’s
Source: history.nasa.gov/ SP-349/ch3.htm
Power
• 378 kW required
• 400kW generated
System Power Required (kW)
Propulsion 352
Attitude Control 2.4
Communications 1
C&DH 1
ECLSS 10
Fuel Generation 3
Thermal 7
ECLSS
• Atmosphere Revitalization System (ARS)
• Active Thermal Control System
• Atmosphere Revitalization Pressure Control System (ARPCS)
• Water Recycling System
• Artificial Gravity?
Scientific Instruments
• Sabatier reactor
– CO2 + 4H2 CH4 + 2H2O
• Electrolysis
– 2H2O 2H2 + O2
• 92,000 kg O2
• 13,000 kg CH4
• Total mass of propellant – 105,000 kg
Future Work
• Integration of all systems into C&DH• MCC, SOCC, POCC located and
defined• More research into C&DH• GNC system chosen• Trade studies for various components of
each system• Artificial Gravity researched