Woven Thermal Protection Systems (WTPS) is a relatively new program funded by the Office of the Chief Technologist (OCT). The WTPS approach to producing TPS architectures uses precisely engineered 3-D weaving techniques that allow tailoring material characteristics needed to meet specific mission requirements. A series of mechanical tests were performed to evaluate performance of different weave types, and get a better understanding of failure modes expected in these three-dimensional architectures. These properties will aid in material down selection and guide selection of the appropriate WTPS for a potential mission
Exploration of ballistic coefficient and entry flight path angle to determine loom requirements for ...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
Issued as Status report, Interim status report and Final report, Project no. E-27-61
Three Dimensional Woven thermal protection system (TPS) materials are one of the enabling technologi...
Woven thermal protection system (TPS) materials are one of the enabling technologies for mechanicall...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
NASA Ames Research Center is developing Woven Thermal Protection System (WTPS) materials as a new cl...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
The Heat Shield for Extreme Entry Environment Technology (HEEET) project seeks to mature a game chan...
Thermal Protection System (TPS) modeling requires accurate representation and prediction of the ther...
A primary focus of the Entry Systems and Technology Division at NASA Ames is design, development, qu...
The Thermal Protection System Materials (TPSM) Project consists of three distinct project elements: ...
NASA and its contractors have completed a program to develop a basic mechanics underpinning for text...
The process of designing a thermal protection system for an entry vehicle involves many stages, incl...
The effort, which was focused on the research and development of advanced materials for use in Therm...
Exploration of ballistic coefficient and entry flight path angle to determine loom requirements for ...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
Issued as Status report, Interim status report and Final report, Project no. E-27-61
Three Dimensional Woven thermal protection system (TPS) materials are one of the enabling technologi...
Woven thermal protection system (TPS) materials are one of the enabling technologies for mechanicall...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
NASA Ames Research Center is developing Woven Thermal Protection System (WTPS) materials as a new cl...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
The Heat Shield for Extreme Entry Environment Technology (HEEET) project seeks to mature a game chan...
Thermal Protection System (TPS) modeling requires accurate representation and prediction of the ther...
A primary focus of the Entry Systems and Technology Division at NASA Ames is design, development, qu...
The Thermal Protection System Materials (TPSM) Project consists of three distinct project elements: ...
NASA and its contractors have completed a program to develop a basic mechanics underpinning for text...
The process of designing a thermal protection system for an entry vehicle involves many stages, incl...
The effort, which was focused on the research and development of advanced materials for use in Therm...
Exploration of ballistic coefficient and entry flight path angle to determine loom requirements for ...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
Issued as Status report, Interim status report and Final report, Project no. E-27-61