Abstract: NASA is developing thin-film based, deployable propulsion, power, and communication systems for small spacecraft that…
Author: New NASA STI
Time Domain Stability Margin Assessment of the NASA Space Launch System GN&C Design for Exploration Mission One
Abstract: The baseline stability margins for NASA's Space Launch System (SLS) launch vehicle were generated via…
Modeling Meteor Flares for Spacecraft Safety
Abstract: NASA's Meteoroid Environment Office (MEO) is tasked with assisting spacecraft operators and engineers in quantifying…
The Conceptual Design of an Electric Sail Technology Demonstration Mission Spacecraft
Abstract: No abstract available
Predictive Simulation of Gas Adsorption in Fixed-Beds and Limitations due to the Ill-Posed Danckwerts Boundary Condition
Abstract: The 1-D axially dispersed plug flow model is a mathematical model widely used for the…
Conceptual Design of an Electric Sail Technology Demonstration Mission Spacecraft
Abstract: There is great interest in examining the outer planets of our solar system and Heliopause…
Time Domain Stability Margin Assessment of the NS Space Launch System GN&C Design for Exploration Mission One
Abstract: The baseline stability margins for NASA's Space Launch System (SLS) launch vehicle were generated via…