Team A, Power Group Presentation

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Presentation transcript:

Team A, Power Group Presentation Patrick Kennedy 1 / 16 / 01

Power Considerations HAB in transit to Mars HAB on surface of Mars Backup power HAB on surface of Mars Rovers on Mars Communication

HAB in Transit NASA plan: 30 kWe Sources considered Nuclear Fission Solar Arrays Fuel Cells Batteries Radioisotope Thermoelectric Generators (RTGs)

HAB in Transit (cont.) Primary selection: Solar Power Good power level Proven concept Backup selection: Regenerative Fuel Cells (RFC)

HAB on Surface NASA plan: 160 kWe Same sources considered as in transit Primary selection: Nuclear fission Great power level Good weight, size Backup selection: Solar Array/RFC Same system used in transit Less reliance on sunny day

Rovers 2 Rovers considered Sources considered Distance rover for multi-day trips Local rover for 1-day trips Sources considered Methane Engine Solar Arrays Fuel Cells Batteries Radioisotope Thermoelectric Generators (RTGs)

Rovers (cont.) Distance Rover NASA plan: 10 kWe Source: Methane Engine Good power Good weight, size Local Rover Lunar Rover: 1 kWe Source: RFCs Good size, weight Recharge from HAB power

Communication Antenna on main craft Source: Use power from HAB’s power source Antenna on separate craft Source: Solar Power Proven design

About the group Related Classes Computer Skills AAE 590K – Advanced Energy Conversion AAE 490E – Intro to Satellite Systems AAE 539 – Advanced Rocket Propulsion (currently enrolled) AAE 490 – Trans-Atmospheric Vehicle Design Computer Skills Matlab (of course) Fortran Some C AutoCAD