1. Final Slides By: Kara Akgulian Mission Ops Locomotion Phase 1

2. Selecting the Capture Orbit 2 Lunar Capture Orbit Altitude 100g and 10kg using Falcon 9 Arbitrary using Falcon 9 Circular Orbit (km)50453525 Total Prop Used (kg)78.9278.7778.4778.16 Savings from 50km (kg) 0.150.450.76 Orbit StabilityStable Circular Orbit (km)50453525 Total Prop Used (kg)1420.601417.901412.501406.90 Savings from 50km (kg) 2.708.101.01 Orbit StabilityStable This will optimize mass savings. Any lower altitude and there is the possibility of crashing into high peaks in the Lunar terrain.

3. Landing Site 3 Mare Cognitum Southeast of Apollo 12 Landing

4. Trajectory Analysis for Large Payload 4 ParameterValue Payload Mass (kg)3542 Thrust (mN)2118 Mass Flow Rate (mg/s)93.5 Earth Phase Angle (deg)216 Moon Phase Angle (deg)270 Parking Orbit Altitude (km)400 Capture Orbit Altitude (km)25 Initial Mass (kg)9953 Flight Time (days)365

5. Space Ball Components 5 ParameterValue Size38 mm 2 Mass0.1 kg Motor Frequency155 kHz Ultrasonic Vibrating Motor: M-674,164 PILine designed by PI Dust Mitigation System Radiation Hardened Camera ParameterValue Diameter24 mm Length110 mm Mass0.54 kg Underwater Color Camera: N34F by Ahlberg Electronics