CubeSat Technology Past and Present: Current State-Of-The-Art Survey
A Brief Overview of the Effects of Impact Damage to Rocket Motor Cases
NASA Access 2 Space Workshop: Summary Report: Increased Science Return through Rideshare
Synthesizing a New Launch Vehicle Failure Probability Based on Historical Flight Data
Mission Success of U.S. Launch Vehicle Flights from a Propulsion Stage-Based Perspective: 1980-2015
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
LAVA Contribution to HiLiftPW-3
Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay Time
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
Ames Modular Common Spacecraft Bus
Emerging US Space Launch, Trends and Space Solar Power
The Orion Pad Abort 1 (PA-1) Flight Test: A Propulsion Success
Orion Launch Abort System (LAS) Propulsion on Pad Abort 1 (PA-1)
Fiber Optic Sensors for Launch Vehicles Project
Working RideShare for the U Class Payload
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
Low Cost Mars Sample Return Utilizing Dragon Lander Project
Nano-Launcher Technologies, Approaches, and Life Cycle Assessment
Armstrong Research, Technology, and Engineering Accomplishments 2014
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
Making the Case for Reusable Booster Systems: The Operations Perspective
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