Add to ORKGVugraphs are presented on the effect of cruise Mach number on the maximum takeoff weight of the High Speed Commercial Transport (HSCT). Predictions are made of the service life of the aircraft, and the aging effects of various candidate materials are examined. The objective of the study is to develop and evaluate low cost airplane designs by examining alternate structural, material, and manufacturing concepts, for the purpose of advising material suppliers and NASA on desired materials, product forms, and processing techniques
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
Research is in progress to develop flight strategy concepts for avoidance and recovery from microbur...
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
In order to meet the anticipated needs in modeling and analysis of advanced aerospace structures, NA...
A design concept that reduces the size of magnetic bearings is assessed. The small size will enable ...
Present research centers on the development of advanced computational methods for transient simulati...
Expressions for the number of truss components per truss division are presented along with expressio...
This paper discusses the procedure, approach and Rocketdyne CFD results for the optimization of the ...
To better understand the Space Shuttle Main Engine (SSME) startup/shutdown tansients, an airflow tes...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
Integrated airframe/propulsion control system architecture is discussed. The main objectives of the ...
Concerns raised over possible base heating effects on the National Launch System (NLS) 1.5 stage ref...
Computational and experimental studies of the thermal structural behavior of thin panels subjected t...
The elements of the test program for the space suit to be used on Space Station Freedom are noted in...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
Research is in progress to develop flight strategy concepts for avoidance and recovery from microbur...
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
In order to meet the anticipated needs in modeling and analysis of advanced aerospace structures, NA...
A design concept that reduces the size of magnetic bearings is assessed. The small size will enable ...
Present research centers on the development of advanced computational methods for transient simulati...
Expressions for the number of truss components per truss division are presented along with expressio...
This paper discusses the procedure, approach and Rocketdyne CFD results for the optimization of the ...
To better understand the Space Shuttle Main Engine (SSME) startup/shutdown tansients, an airflow tes...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
Integrated airframe/propulsion control system architecture is discussed. The main objectives of the ...
Concerns raised over possible base heating effects on the National Launch System (NLS) 1.5 stage ref...
Computational and experimental studies of the thermal structural behavior of thin panels subjected t...
The elements of the test program for the space suit to be used on Space Station Freedom are noted in...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
Research is in progress to develop flight strategy concepts for avoidance and recovery from microbur...