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An entry trajectory design methodology for lunar return
Zachary R. Putnam
, Gregg H. Barton
, Matthew D. Neave
Research output
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Chapter in Book/Report/Conference proceeding
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Conference contribution
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Keyphrases
Design Methodology
100%
Entry Trajectory
100%
Lunar Return
100%
Trajectory Design
100%
Design Space
75%
Vehicle Engineering
75%
Orion
75%
Lift-to-drag Ratio
75%
Performance Margin
75%
Entry Vehicle
50%
Operations Concepts
50%
Flight Path Angle
50%
Proposed Methodology
25%
Design Parameters
25%
Deceleration
25%
Monte Carlo Analysis
25%
Parameter Analysis
25%
Evaluation Parameters
25%
Hypersonic
25%
Operation Design
25%
Vehicle Performance
25%
Crew Exploration Vehicle
25%
Return-entry
25%
Six Degrees of Freedom Simulation
25%
Aeroheating
25%
Crew Module
25%
Maximize Performance
25%
Engineering
Design Space
100%
Lift to Drag Ratio
100%
Vehicle Design
66%
Flight Path Angle
66%
Design Parameter
33%
Degree of Freedom
33%
NASA
33%
Monte Carlo Analysis
33%