CYCLOIDAL GAIT WITH DOUBLE SUPPORT PHASE FOR THE NAO HUMANOID ROBOT
CYCLOIDAL GAIT WITH DOUBLE SUPPORT PHASE FOR THE NAO HUMANOID ROBOT
Concept of Operations for RCO SPO
21st Century Space Launch Complex
New System for Approaching the Design of Sounding Rockets
Configurable Technology Development for Reusable Control and Monitor Ground Systems
Reusable Launch Vehicle Development Research
Technologies Involved in Configuring an Advanced Earth-to-Orbit Transport for Low Structural Mass
Use of the Collaborative Optimization Architecture for Launch Vehicle Design
Project Antares: A Low Cost Modular Launch Vehicle for the Future
Structural Sizing of a 25,000-lb Payload, Air-Breathing Launch Vehicle For Single-Stage-To-Orbit
Advanced Transportation System Studies Technical Area 2(TA-2): Heavy Lift Launch Vehicle Development