Add to ORKGAn analytical model was developed that can be used to establish certain parameters of a thermal vacuum environmental test program based on an optimization of program costs. This model is in the form of a computer program that interacts with a user insofar as the input of certain parameters. The program provides the user a list of pertinent information regarding an optimized test program and graphs of some of the parameters. The model is a first attempt in this area and includes numerous simplifications. The model appears useful as a general guide and provides a way for extrapolating past performance to future missions
Early design studies showed that the UV spectrometer thermal design margins were very small so that ...
Analysis techniques to evaluate the effects of changing thermal loads and the methods utilized to co...
Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unma...
The thermal vacuum test optimization model developed to provide an approach to the optimization of a...
The Apollo Telescope Mount's thermal systems unit was utilized to conduct a full-scale thermal vacuu...
For space flight hardware, the thermal vacuum environmental test is the best test of a system's flig...
This work discusses the modification and analysis of the Blue Thermal Vacuum Chamber (TVAC) located ...
A thermal vacuum test was performed on the engineering model of the outer planets atmospheric entry ...
This thesis describes the development and correlation of a thermal model that forms the foundation ...
This thesis describes the development and correlation of a thermal model that forms the foundation o...
The purpose of this senior project is to understand the capabilities of the thermal vacuum chamber i...
Spacecraft are subject to different environments while on orbit around the Earth and beyond. One of ...
In space industry thermal models are an important tool to predict, analyze and understand the therma...
A thermal stress analysis is an important aspect in the design of aerospace structures and vehicles ...
Test procedure development for high-intensity thermal testing of solar probe spacecraf
Early design studies showed that the UV spectrometer thermal design margins were very small so that ...
Analysis techniques to evaluate the effects of changing thermal loads and the methods utilized to co...
Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unma...
The thermal vacuum test optimization model developed to provide an approach to the optimization of a...
The Apollo Telescope Mount's thermal systems unit was utilized to conduct a full-scale thermal vacuu...
For space flight hardware, the thermal vacuum environmental test is the best test of a system's flig...
This work discusses the modification and analysis of the Blue Thermal Vacuum Chamber (TVAC) located ...
A thermal vacuum test was performed on the engineering model of the outer planets atmospheric entry ...
This thesis describes the development and correlation of a thermal model that forms the foundation ...
This thesis describes the development and correlation of a thermal model that forms the foundation o...
The purpose of this senior project is to understand the capabilities of the thermal vacuum chamber i...
Spacecraft are subject to different environments while on orbit around the Earth and beyond. One of ...
In space industry thermal models are an important tool to predict, analyze and understand the therma...
A thermal stress analysis is an important aspect in the design of aerospace structures and vehicles ...
Test procedure development for high-intensity thermal testing of solar probe spacecraf
Early design studies showed that the UV spectrometer thermal design margins were very small so that ...
Analysis techniques to evaluate the effects of changing thermal loads and the methods utilized to co...
Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unma...