This report is a description of the 14 x l4-Inch Trisonic Wind Tunnel facility at the Marshall Space Flight Center and is published as a handbook for the potential user of the facility who is not otherwise familiar with its operation. The following items are presented to illustrate the capabilities and operation of the tunnel: (1) facility description, (2) performance and operational characteristics, (3) model design, (4) instrumentation and data recording equipment, (5) data processing and presentation, and (6) preliminary test information required
A computer graphics simulation of an aircraft Head-Up Display was designed using an RDS-3000 Ikonas ...
The aim of this thesis is to obtain from a simulation procedure a set of graphs to compute the numbe...
Instrumentation and a new valving system is designed and built for use with an expansion type cloud ...
The work performed by the Attitude Determination and Control Section at the National Aeronautics and...
The Tracking and Data System, which provided outstanding support to the Mariner Venus/Mercury 1973 p...
The analytical models and results of a structural dynamics investigation of the reference initial op...
This report discusses the application and cost of two types of altimeter systems (spaceborne (satell...
Feasibility of trajectory guidance and control concept for lifting configuration with roll modulatio
The Lewis Research Center's Hybrid Simulation Lab contains a collection of analog, digital, and hybr...
Dr. Sherman P. Vinograd fulfilled the roles of Chief of Medical Science and Technology and Director ...
The effectiveness of incroporating a real-time oculometer system into a Boeing 737 commercial flight...
The development of a digital, three dimensional, automatic control law designed to achieve an optima...
The Z80 microprocessor based computer program that directs and controls the operation of the six cha...
Considerable data on various parameters of a satellite and its launching vehicle can be obtained fro...
The details are presented of an onboard digital computer algorithm designed to reliably detect and i...
A computer graphics simulation of an aircraft Head-Up Display was designed using an RDS-3000 Ikonas ...
The aim of this thesis is to obtain from a simulation procedure a set of graphs to compute the numbe...
Instrumentation and a new valving system is designed and built for use with an expansion type cloud ...
The work performed by the Attitude Determination and Control Section at the National Aeronautics and...
The Tracking and Data System, which provided outstanding support to the Mariner Venus/Mercury 1973 p...
The analytical models and results of a structural dynamics investigation of the reference initial op...
This report discusses the application and cost of two types of altimeter systems (spaceborne (satell...
Feasibility of trajectory guidance and control concept for lifting configuration with roll modulatio
The Lewis Research Center's Hybrid Simulation Lab contains a collection of analog, digital, and hybr...
Dr. Sherman P. Vinograd fulfilled the roles of Chief of Medical Science and Technology and Director ...
The effectiveness of incroporating a real-time oculometer system into a Boeing 737 commercial flight...
The development of a digital, three dimensional, automatic control law designed to achieve an optima...
The Z80 microprocessor based computer program that directs and controls the operation of the six cha...
Considerable data on various parameters of a satellite and its launching vehicle can be obtained fro...
The details are presented of an onboard digital computer algorithm designed to reliably detect and i...
A computer graphics simulation of an aircraft Head-Up Display was designed using an RDS-3000 Ikonas ...
The aim of this thesis is to obtain from a simulation procedure a set of graphs to compute the numbe...
Instrumentation and a new valving system is designed and built for use with an expansion type cloud ...