Add to ORKGThree minimizing techniques are evaluated to determine the most efficient method for minimizing the weight of a thermal protection system and for reducing computer usage time. The methods used (numerical optimization and nonlinear least squares) for solving the minimum-weight problem involving more than one material and more than one constraint are discussed. In addition, the one material and one constraint problem is discussed
A method for integrating Aeroheating analysis into conceptual reusable launch vehicle RLV design is ...
A thermal optimality criterion is presented for sizing members of heated structures with multiple te...
AIAA Space 2000 Conference and Exposition Long Beach, CA, September 19-21, 2000.This paper outlines...
Computational techniques were developed and assimilated for the design optimization. The resulting c...
A modular program for design optimization of thermal protection systems is discussed. Its capabiliti...
The development of the computational techniques for the design optimization of thermal protection sy...
A new MATLAB-based program called TOP 2 was developed as an alternative tool for the Fortran program...
The purpose of thermal protection system (TPS) is to maintain the structural temperature of the hype...
The integrated thermal protection system (ITPS) is a complicated system that addresses both mechanic...
peer-reviewedThe integrated thermal protection system (ITPS) is a complicated system that addresses ...
A finite-element based procedure is described for obtaining minimum mass designs of structures subje...
During its lifetime a space launcher is subjected to extreme heat loads. To protect space vehicles f...
A program was conducted to develop a lightweight, efficient metallic thermal protection system (TPS)...
Nonlinear least squares techniques can be used to determine effective thermal conductivity values fr...
The benefits of nuclear thermal propulsion are numerous and relevant to the current NASA mission goa...
A method for integrating Aeroheating analysis into conceptual reusable launch vehicle RLV design is ...
A thermal optimality criterion is presented for sizing members of heated structures with multiple te...
AIAA Space 2000 Conference and Exposition Long Beach, CA, September 19-21, 2000.This paper outlines...
Computational techniques were developed and assimilated for the design optimization. The resulting c...
A modular program for design optimization of thermal protection systems is discussed. Its capabiliti...
The development of the computational techniques for the design optimization of thermal protection sy...
A new MATLAB-based program called TOP 2 was developed as an alternative tool for the Fortran program...
The purpose of thermal protection system (TPS) is to maintain the structural temperature of the hype...
The integrated thermal protection system (ITPS) is a complicated system that addresses both mechanic...
peer-reviewedThe integrated thermal protection system (ITPS) is a complicated system that addresses ...
A finite-element based procedure is described for obtaining minimum mass designs of structures subje...
During its lifetime a space launcher is subjected to extreme heat loads. To protect space vehicles f...
A program was conducted to develop a lightweight, efficient metallic thermal protection system (TPS)...
Nonlinear least squares techniques can be used to determine effective thermal conductivity values fr...
The benefits of nuclear thermal propulsion are numerous and relevant to the current NASA mission goa...
A method for integrating Aeroheating analysis into conceptual reusable launch vehicle RLV design is ...
A thermal optimality criterion is presented for sizing members of heated structures with multiple te...
AIAA Space 2000 Conference and Exposition Long Beach, CA, September 19-21, 2000.This paper outlines...