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
Low Thrust Cis-Lunar Transfers Using a 40 kW-Class Solar Electric Propulsion Spacecraft
Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay Time
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
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
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)
Lifting center-body land recoverable booster concept.
Study of optimal and adaptive control theory Final report, May 1964 - Jun. 1966
Optimal payload trajectory characteristics for winged booster vehicles.
Improvements in stage checkout
Lunar orbit mission analysis for the improved Delta launch vehicle and AIMP-D SPACECRAFT
Integrated reliability program for Scout research vehicle.
Analysis and Design of Space Vehicle Flight Control Systems. Volume I - Short Period Dynamics
Design and fabrication considerations for a 1/10-scale replica model of the Apollo/ Saturn V