Implicit ablation and thermal response software was developed to analyse and size charring ablative thermal protection systems for entry vehicles. A statistical monitor integrated into the tool, which uses the Monte Carlo technique, allows a simulation to run over stochastic series. This performs an uncertainty and sensitivity analysis, which estimates the probability of maintaining the temperature of the underlying material within specified requirements. This approach and the associated software are primarily helpful during the preliminary design phases of spacecraft thermal protection systems. They are proposed as an alternative to traditional approaches, such as the Root-Sum-Square method. The developed tool was verified by comparing the...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
Mass estimating relationships (MERs) are developed to predict the amount of thermal protection syste...
A computer tool to perform entry vehicle ablative thermal protection systems sizing has been develop...
AIAA Aerospace Sciences Conference January 2006, Reno, NV.A computer tool to perform entry vehicle ...
Ablative materials are often used for spacecraft heatshields to protect underlying structures from t...
This paper presents a probabilistic analysis methodology for a nonablative thermal protection system...
Atmospheric entry vehicle thermal protection systems are margined due to the uncertainties that exis...
Accurate characterization of Thermal Protection System (TPS) material properties is an important com...
System analysis and design of any entry system must balance the level fidelity for each discipline a...
The Orion Thermal Protection System (TPS) margin process uses a root-sum-square approach with branch...
During hypersonic trajectory through a planetary atmosphere a high heat flux environment is generate...
The process of designing a thermal protection system for an entry vehicle involves many stages, incl...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
During its lifetime a space launcher is subjected to extreme heat loads. To protect space vehicles f...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
Mass estimating relationships (MERs) are developed to predict the amount of thermal protection syste...
A computer tool to perform entry vehicle ablative thermal protection systems sizing has been develop...
AIAA Aerospace Sciences Conference January 2006, Reno, NV.A computer tool to perform entry vehicle ...
Ablative materials are often used for spacecraft heatshields to protect underlying structures from t...
This paper presents a probabilistic analysis methodology for a nonablative thermal protection system...
Atmospheric entry vehicle thermal protection systems are margined due to the uncertainties that exis...
Accurate characterization of Thermal Protection System (TPS) material properties is an important com...
System analysis and design of any entry system must balance the level fidelity for each discipline a...
The Orion Thermal Protection System (TPS) margin process uses a root-sum-square approach with branch...
During hypersonic trajectory through a planetary atmosphere a high heat flux environment is generate...
The process of designing a thermal protection system for an entry vehicle involves many stages, incl...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
During its lifetime a space launcher is subjected to extreme heat loads. To protect space vehicles f...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
The current status of aerothermal and thermal protection system modeling for civilian entry missions...
Mass estimating relationships (MERs) are developed to predict the amount of thermal protection syste...