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Georgia Institute of Technology
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iconBelow is a list of Masters Projects produced within SSDL. These papers are available for download in Adobe Acrobat pdf file format. These papers are copyrighted. They are intended for the use of individual researchers in the field.arrow

icon Masters Project: 2009

icon Brinckerhoff, A.T.; Russell, R.P.
Resonance Hopping Transfers Between Moon Science Orbits
April 2009

icon Chua, Z.; Braun, R.D.; Feigh, K.M.
Analysis of Human-System Interaction for Landing Point Redesignation
May 2009

icon Cordell, C.; Braun, R.D.
Computational Fluid Dynamics Validation of a Single Central Nozzle Supersonic Retropropulsion Configuration
May 2009

icon Hutchings, A.; Braun, R.D.
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
May 2009

icon Marsh, C.; Braun, R.D.
Fully-Propulsive Mars Atmospheric Transit Strategies for High-Mass Missions
April 2009


icon Masters Project: 2008

iconSmith, P.J.; Braun, R.D.
Parametric Analysis and Targeting Capabilities for the Planetary Entry Systems Synthesis Tool
December 2008

iconKorzun, A.; Braun, R.D.
Supersonic Retropropulsion Technology for Application to High Mass Mars Entry, Descent, and Landing
May 2008

iconSteinfeldt, B.; Braun, R.D.
Guidance, Navigation, and Control Technology System Trades for Mars Pinpoint Landing
May 2008

iconGrant, M.; Braun, R.D.
Smart Divert: A New Entry, Descent, and Landing Architecture
May 2008

iconFlaherty, K.; Braun, R.D.
Initial Implementation of a Adjoint CFD Code for Aeroshell Shape Optimization
May 2008


iconMasters Project: 2007

icon Theisinger, J.; Braun, R.D.
Hypersonic Entry Aeroshell Shape Optimization
December 2007

icon Stahl, B. A.; Braun, R.D.
Low-Thrust Trajectory Optimization Tool to Assess Options for Near-Earth Asteroid Deflection
December 2007

icon Kranzusch, K. M.; Braun, R.D.
Space Shuttle Solid Rocket Booster Control Limitations Due to Failure of an Hydraulic Power Unit
November 2007

icon Christian, J.; Braun, R.D.
Statistical Reconstruction of Mars Entry, Descent, and Landing Trajectories and Atmospheric Profiles
May 2007


iconMasters Project: 2006

iconClark, I.; Braun, R.D.
An Evaluation of Ballute Entry Systems for Lunar Return Missions
May 2006

iconLantoine, G.; Braun, R.D.
Optimal Trajectories for Soft Landing on Asteroids
May 2006

iconFrancis, S.; Braun, R.D.
Entry Systems Design of the Mars Gravity Biosatellite
May 2006

iconThompson, R.; Wilhite, A.
Performance Evaluation of a Side Mounted Shuttle Derived Heavy Lift Launch Vehicle for Lunar Exploration
May 2006

iconStreet, D.; Wilhite, A.
A Scalable Orbital Propellant Depot Design
May 2006

iconWells, G.; Braun, R.D.
Mars Entry, Descent and landing Parametric Trades Full Version (100MB)
May 2006


iconMasters Project: 2005
iconHellman, B.; Olds, J.
Comparison of Return to Launch Site Options for a Reusable Booster Stage
August 2005

iconAlemany, K.; Olds, J.
Comparison of An Expendable and Reusable Lunar Exploration Architecture Using Lunar Architecture Stochastic Simulator and Optimizer
May 2005

iconYoung, J.; Olds, J.
Probabilistic Assessment of the Space Tourism Industry: What will it take to Make it Profitable?
May 2005

iconKohei, T.; Olds, J.
Conceptual Design and Analysis of a Small and Low-Cost Launch Vehicle (Microcosm Sprite Test Model)
May 2005

iconKipp, D.; Braun, R.D. Development of Trajectory Simulation Capabilities for the Planetary Entry Systems Synthesis Tool.
May 2005

iconPrakash, R.; Braun, R.D.
Comparison of Transition to Flight Methods for a Titan Helicopter
May 2005

iconTaya, Kohei; Olds, J.
Conceptual Design and Analysis of a Small and Low-Cost Launch Vehicle (Microcosm Sprite Test Model)
Spring 2005


iconMasters Project: 2004
iconReeves, J.; Olds, J.
Discrete Event Simulation of Reusable launch Vehicle Ground Operations
July 2004

iconBrown, N.; Olds, J.
Evaluation of Multidisciplinary Optimization techniques Applied to a Reusable Launch Vehicle
May 2004

iconCrowley, J.; Olds, J.
Design, Modeling, and Simulation of a Hydrogen-Induced Air Liquefaction System Applicable to Space Access Vehicles
May 2004

iconHutchinson, V.; Olds, J.
Analytical Structural Weight of Conceptual Launch Vehicle Fuselage Components with the Georgia tech Structural Tool for Rapid Estimation of Shell Sizes (GT-STRESS)
May 2004

iconPimentel, J.; Olds, J.
Development of An Online Database Tool for Quick Access to Mass Estimating Relationships
May 2004

iconYoung, D.; Olds, J.
Responsive Access Small Cargo Affordable Launch (RASCAL) Independent Performance Evaluation
May 2004

iconKrevor, Z.; Olds, J.
A Case Study of the STS Indirect and Support Costs
May 2004


iconMasters Project: 2003

iconKeisner, A.; Olds, J.
Reliability Analysis Technique Comparison, as Applied to the Space Shuttle
December 2003

iconSteffes, S.; Olds, J.
Magel: An Advanced Partially Reusable launch Architecture Concept
December 2003


iconMasters Project: 2002
iconStaton, E.; Olds, J.
Developing the Operational Requirements for the Next generation launch Vehicle Spaceport
April 2002

iconRohrschneider, R.; Olds, J.
Development of a Mass Estimating Relationship Database for Launch Vehicle Conceptual Design
April 2002

iconMiller, J.; Olds, J.
Investigation of Transonic Drag Computations in Aerodynamic Preliminary Analysis Systems (APAS)
April 2002

iconGrillmayer, G.; Olds, J.
Space Launch Vehicle Trajectory Optimization using the Weak Hamiltonian Finite Element Method for Optimal Control
Fall 2002


iconMasters Project: 2001
iconMarcus, L.; Olds, J.
Generating Physic=based Mass Estimating Relationship: A test case Using-LOX-Tank bending Loads Applied to the Forward LH2 Tank of the Georgia Tech Air Breathing Launch Vehicle
December 2001

iconIzon, S; Olds, J.
Improvements in Thermal Protection System Sizing Capabilities for TCAT
December 2001

iconLee, S.; Olds, J.
Reliabilty Drivers or Advanced Space Vehicles
July 2001

iconScott, A.; Olds, J.
An Evaluation of Three Commercially Available Integrated Design Frameworks Packages for use in the Space Systems Design Lab
April 2001

iconNelson, D.; Olds, J.
Qualitative and Quantitative Assessment of Optimal Trajectories by Implicit Simulations (OTIS) and program to Optimize Simulated Trajectories (POST)
April 2001

iconCormier, T.; Olds, J.
PHATCAT: Power-Head and Thrust Chamber Analysis Tool
Fall 2001

iconWeglian, J.; Olds, J.
Trajectory Animator JAVA Applet
Fall 2001

iconBechtel, R.; Olds, J.
T-BEAT: Turbine-based Engine Analysis Tool
Summer 2001


iconMasters Project: 2000

iconCharania, A.C.; Olds, J.
Evaluation of a Technique for Prioritizing Technology Investment for Advanced Space Transportation Systems
Summer 2000


iconMasters Project: 1999

iconSorensen, K.; Olds, J.
Comparison of CFD with APAS Aerodynamic Results for Stargazer, a Bantam-class RLV
Fall 1999

iconTooley, J.; Olds, J.
Performance Evaluation of Bimese RLV for Commercial Payload Missions
Fall 1999


iconMasters Project: 1998

iconScott, J.; Olds, J.
Modeling Large Aerodynamic Datasets with Response Surfaces
Fall 1998

iconActon, D.; Olds, J.
Computational Frameworks for Launch Vehicle Design
Spring 1998

iconSteadman, K.; Olds, J.
Cross-Platform Techniques for Code Integration and Optimization
Spring 1998


iconMasters Project: 1997

iconBellini, P.; Olds, J.
I-DEAS to APAS Geometry File Translation
Fall 1997

iconLee, H.; Olds, J.
A Computational Tool for Cost Modeling and Business Simulation in Launch Vehicle Design
Summer 1997

iconMcGinnis, P.; Olds, J.
Development and Derivation of Equations for Scramjet Engine Modeling
Spring 1997

iconSaks, G.; Olds, J.
A Computational Tool for RBCC EnginBC
Spring 1997





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8/28/05