Alternatives Concepts White Paper IPT 02E
The University of Alabama Huntsville Project Management The University of Alabama Huntsville Team Leader Eddie Kiessling Structures Nathan Coffee Systems Engineer Jay Gala GN & C Brandon York Joseph Sandlin Operations Brett Guin Thermal Kathryn Kirsh Payload Operations Brent Newson Power Christopher Goes Technical Editor Michael Bryan
Overview
Technical Description Overview of Phase 2: Deliverable Items: White Paper Summarizes the strategy for selecting alternative systems Qualitative/quantitative information to evaluate each idea Logical rational for down selecting one concept among the three concepts Oral Presentation Summarizing information from the White Paper to present to the review board.
Technical Description Specification Summary Level 1 Requirements Housed within an Atlas V-401 EPF Shroud Total Landed Mass – 997.4 kg Launch Date – NLT September 30, 2012 Survivability Time of 1 Year Attain a slope of 12º Polar Landing as well as other Lunar Landings Land Precision +/- 100 3σ Maneuverability SMD to ESMD
Specification Summary
Team Eclipse Approach to Phase 2
Description of Concepts Viking Lander (Baseline Design) Lander on Wheels (Concept 1) Lander + Rover (Concept 2) Selection Process Pros and Cons Weighting of FOMs Analysis and Comparison Concept Chosen: Lander on Wheels (Concept 1)
Boost Matrix for Project 02
02-BL “Viking”
02E-ALT1 “Lander on Wheels”
02E-ALT2 “Lander + Rover”
Selection of Final Concept
Illustrations
Illustrations
Engineering Summary
Phase 3 Plan
Review