Amorphous carbonaceous char produced from the pyrolysis of polymer solids has many desirable properties for ablative heat shields for space vehicles. Molecular dynamics simulations are presented to study the transformation of the local atomic structure from virgin polymer to a dense, disordered char [1]. Release of polymer hydrogen is found to be critical to allow the system to collapse into a highly coordinated char structure. Mechanisms of the char formation process and the morphology of the resulting structures are elucidated. Thermal conductivity and mechanical response of the resulting char are evaluated [2]. During reenty, the optical response and oxidative reactivity of char are also important properties. Results of ab initio computa...
A mimetic method based on Monte Carlo simulation is proposed to generate a molecular model of char. ...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Ablative materials are used in heat shields of spacecrafts re-entering the atmosphere to protect the...
The thermal protection materials used for spacecraft heat shields are subjected to various thermal a...
Molecular structure effects on thermochemical properties of phenolic resins and related polymer
During the reentry of aerospace vehicles into the earth\u27s atmosphere, the outer shell surface tem...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Charring thermal protection systems have been used to protect hypersonic vehicles from high heat loa...
A simulation technique has been developed for predicting the char yield of organic resins during hig...
We examine the mechanism of pyrolysis and charring of large (> 10,000 atom) phenol-formaldehyde resi...
The decomposition of ablative composites is described along with the transport phenomena of pyrolysi...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Charring thermal protection systems have been used to protect hypersonic vehicles from high heat ...
During terrestrial atmospheric re-entry, aerospace vehicles can be subjected to temperatures greater...
A mimetic method based on Monte Carlo simulation is proposed to generate a molecular model of char. ...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato
Ablative materials are used in heat shields of spacecrafts re-entering the atmosphere to protect the...
The thermal protection materials used for spacecraft heat shields are subjected to various thermal a...
Molecular structure effects on thermochemical properties of phenolic resins and related polymer
During the reentry of aerospace vehicles into the earth\u27s atmosphere, the outer shell surface tem...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
Charring thermal protection systems have been used to protect hypersonic vehicles from high heat loa...
A simulation technique has been developed for predicting the char yield of organic resins during hig...
We examine the mechanism of pyrolysis and charring of large (> 10,000 atom) phenol-formaldehyde resi...
The decomposition of ablative composites is described along with the transport phenomena of pyrolysi...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Charring thermal protection systems have been used to protect hypersonic vehicles from high heat ...
During terrestrial atmospheric re-entry, aerospace vehicles can be subjected to temperatures greater...
A mimetic method based on Monte Carlo simulation is proposed to generate a molecular model of char. ...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablato