Optimization of Inflatable Spacecraft Interior Volume Using Constraints Driven Design
40th International Conference on Environmental Systems
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Combined Stresses , Mathematical Models , National Aeronautics and Space Administration , Integrated Development Environments , Inflatable Spacecraft , Pro/ENGINEER , Heavy Lift Launch Vehicle , International Space Station , Computer Aided Manufacturing , Environmental Control and Life Support System
Optimization of Inflatable Spacecraft Interior Volume Using Constraints Driven Design
British Library Conference Proceedings | 2010
|Constraints Driven Design of a Surface Inflatable Habitat Module
SAE Technical Papers | 2006
|Foam-Reinforced Inflatable Spacecraft
Online Contents | 1997
Inflatable Spacecraft using "Rigidization-on-Command" Concept
British Library Conference Proceedings | 2000
|