Embry Riddle Final

Professor: Dr. Bogdan Udrea Team Lead: Robert Latta Team Members: David Paiz Brandon Walsh-Reed Svilen Kozhuharov Mathieu Naslin Johann Schrell

Overview ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Financial Excellence History ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Financial Excellence Immediate Funding ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Financial Excellence USD Budget $26.14 Million Total Project Cost $10 Mil Launch $1 Mil OBC $0.14 Mil Engineers $1 Mil Telecom $1 Mil Structures $1 Mil Power $5 Mil Software development $2 Mil Cameras and lidar (procurement) $5 Mil Throttable rocket engines COST COMPONENT

Financial Excellence Sustainable Funding ,[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Trajectory Trade-Offs ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Lunar Transfer Trajectories Figure 7‑42: LEO to Moon at 180 o Figure 7‑64: LEO Arrival to Moon at 180 o

Technical Excellence Lunar Transfer Trajectories Figure 7-15: Arrival at Moon and Landing Figure 7-13: Bi-Elliptic Transfer Figure 7-14: Arrival to the Moon’s Sphere of Influence

Technical Excellence Lunar Transfer Trajectories Figure 7‑182: Successful WSB Trajectory from LEO

Technical Excellence MATLAB Code 3.103 5.66 3.155 5.571 5.613 TOTAL Δv (km/s) 90 55 4.65 120 4.63 Time of Flight (days) 2.374 First Maneuver 3.15 Second Maneuver 0.1355 GTO Bi-elliptic (Moon fly-by) 2.39 2.48 2.39 2.502 Landing Δv (km/s) .713 GTO WSB (Moon fly-by) 0.6745 GTO Direct 3.181 LEO WSB 3.111 LEO Direct TLI Δv (km/s) Trans-lunar Trajectory

Technical Excellence From the Earth to the Moon Earth Moon STAR 13B Stage 1 STAR 13B Stage 2 Craft Launcher Payload Fairing

Technical Excellence Stage 1 ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Stage 2 ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Stage 3 ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence To the Lunar Surface Lunar Surface – South Pole Ignite SRM 35 km, 2.48 km/s SRM Burnout 2 km, 0.11 km/s + Craft Separation Horizon acquisition and lateral motion cancellation Hazard avoidance Liquid engine cutoff, 1 m

Technical Excellence Subsystems ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Instruments Spectrometer ,[object Object],[object Object],[object Object],[object Object],100mm 50mm 25mm

Instruments Altimeter ,[object Object],[object Object],[object Object],Courtesy: JPL

Instruments Camera ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Courtesy: Rocketcam DVS

Instruments Inertia Measurement Device ,[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Locomotive

Instruments Mass Budget 15 Dry weight 0.5 Science package 0.4 Payload 0.5 Thermal control system 0.5 Attitude control thrusters 1 GNC package 0.65 Onboard computer 1.5 Tanks (pressurant + hydrazine) 1 Telecom 3 Structures 1.75 Power unit (batteries, wiring, solar panels) 0.2 Cameras + baffles 4 Throttable rocket engines + mounting TOTAL COMPONENT MASS (Kg) COMPONENT

Technical Excellence Mooncasts ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Mooncasts ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence Mooncasts ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Technical Excellence XPF Payload ,[object Object],[object Object]

Technical Excellence Ethical and Legal Issues ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Summary ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Embry Riddle Final

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