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Ideal Operating Time for Minimized Power System

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Presentation on theme: "Ideal Operating Time for Minimized Power System"— Presentation transcript:

1 Ideal Operating Time for Minimized Power System
Rover Power Ideal Operating Time for Minimized Power System [Jeff Knowlton] [Power] 1

2 [Jeff Knowlton] [Power]
Solar Panel 0.09m2 Max output 38 watts Battery 40Watt-hours Can run the rover for 1.1 Hours ( Not transmitting) Dictating time from deployment to time entering the sun [Jeff Knowlton] [Power] 2

3 [Jeff Knowlton] [Power]
86 hours of positive return [Jeff Knowlton] [Power] 3

4 [Jeff Knowlton] [Power]
Assumptions CPU, thermal controls and motors run continuously Mare Cognitum landing sight 3 degrees south of Equator Waiting in Lander for optimal departing time Power use for transmitting takes less than five second for all required components [Jeff Knowlton] [Power] 4

5 Initial Power Use Values
CPU -5 watts Thermal -20 watts (2.5 safety factor) Driving motors – 10 watts (1.08 safety factor) Camera-18 watts(Video camera not yet still camera) Transmitter watts Antenna-0.2 watts [Jeff Knowlton] [Power] 5

6 [Jeff Knowlton] [Power]
Maximum drive time: 86 hours Ideal Deployment 130 hours after daybreak Reduced to 72 hours for mission completion cushion (Safety factor 8) Maximum permanent angle displacement:19.5 degrees 15 degrees permanent slope 3 degrees landing sight 1.5 degrees lunar axis tilt 1.6 watt surplus 4 hour survival on 45 % incline [Jeff Knowlton] [Power] 6

7 [Jeff Knowlton] [Power]
Transmitting costs (18w+6.25w+0.2w)*5(second)*5(transmissions per hour)/3600(seconds per hour) watt-hours [Jeff Knowlton] [Power] 7

8 [Jeff Knowlton] [Power]
Note 3600 watts is 1 watt-hour By comparison the battery is 40 watt hours Not including possible angle offset [Jeff Knowlton] [Power] 8


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