NASA Access 2 Space Workshop: Summary Report: Increased Science Return through Rideshare
Optimal Reference Strain Structure for Studying Dynamic Responses of Flexible Rockets
Low Thrust Cis-Lunar Transfers Using a 40 kW-Class Solar Electric Propulsion Spacecraft
Overview of the Mission Design Reference Trajectory for NASA's Asteroid Redirect Robotic Mission
Inviscid and Viscous CFD Analysis of Booster Separation for the Space Launch System Vehicle
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Low Cost Mars Sample Return Utilizing Dragon Lander Project
RL10 Engine Ability to Transition from Atlas to Shuttle/Centaur Program
Mars Sample Return Landed with Red Dragon
Modeling Complex Cross-Systems Software Interfaces Using SysML
2011 Mars Science Laboratory Trajectory Reconstruction and Performance from Launch Through Landing
Feasibility of Large Launch Vehicle Recovery
Systems Engineering and Technology Considerations of a Mars Ascent Vehicle
CloudSat Safety Operations at Vandenberg AFB
System, cost, and risk analysis for access to space
Mars Exploration Rovers Launch Performance and TCM-1 Maneuver Design
A Comparison of Transportation Systems for Human Missions to Mars
Launch vehicle accident assessment for Mars Exploration Rover missions
Vehicle Health and Sensors Reusable Launch Vehicle (RLV)
Human Mars Mission: Transportation Assessment
The Manned Transportation System Study: Defining Human Pathways into Space
Systems-planning for transportation of large launch vehicles and spacecraft.
Lifting center-body land recoverable booster concept.
Optimal payload trajectory characteristics for winged booster vehicles.
Integrated reliability program for Scout research vehicle.
Design and construction of ground support equipment for the Apollo/Saturn V lunar landing mission.
Optimization problems caused by interaction of guidance and propellant systems.
Optimization problems caused by interaction of guidance and propellant systems.
A survey of advanced structural technologies applicable to future large launch vehicles.
Stability problems in the control of Saturn launch vehicles.
Powered flight trajectory determination techniques as applied to Saturn V vehicles.
Automatic design of optimum Atlas-Agena vehicle trajectories.
Application of redundancy in the Saturn V guidance and control system.
Systems evaluation of advanced structures and materials in future launch vehicles.
Feasibility and Design Study of an Unguided Solar Orbital Launch Vehicle
Advanced control systems for the Saturn V launch vehicle.
The reliability contribution of the pilot to a large launch vehicle control system.