Andere Kunden interessierten sich auch für
![Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-away-Special Experiment for Spaceflight Qualification]( "Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-away-Special Experiment for Spaceflight Qualification")
Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-away-Special Experiment for Spaceflight Qualification61,99 €![Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX) for Spaceflight Qualification]( "Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX) for Spaceflight Qualification")
Final Assembly, Testing and Processing of the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX) for Spaceflight Qualification60,99 €![Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment]( "Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment")
Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment61,99 €![Rigex: Preliminary Design of a Rigidized Inflatable Get-Away-Special Experiment]( "Rigex: Preliminary Design of a Rigidized Inflatable Get-Away-Special Experiment")
Rigex: Preliminary Design of a Rigidized Inflatable Get-Away-Special Experiment60,99 €![Experimental Vibration Analysis of Inflatable Beams for an AFIT Space Shuttle Experiment]( "Experimental Vibration Analysis of Inflatable Beams for an AFIT Space Shuttle Experiment")
Experimental Vibration Analysis of Inflatable Beams for an AFIT Space Shuttle Experiment61,99 €![Education Through Experience. A Four Year Experiment in the Ethical Culture School]( "Education Through Experience. A Four Year Experiment in the Ethical Culture School")
Education Through Experience. A Four Year Experiment in the Ethical Culture School16,99 €![Some Aspects of the Mechanical Response of PMR-15 Neat Resin at 288oC: Experiment and Modeling]( "Some Aspects of the Mechanical Response of PMR-15 Neat Resin at 288oC: Experiment and Modeling")
Some Aspects of the Mechanical Response of PMR-15 Neat Resin at 288oC: Experiment and Modeling60,99 €
The purpose of this research project is to develop the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX) from a computer-based model into a space-qualified prototype. Past research projects have developed RIGEX's command and control, structural analysis, and integration with the orbiter. This thesis details the organization, assembly, and test planning for the RIGEX protoflight model. Strict requirements imposed by the National Aeronautics and Space Administration (NASA) must be fulfilled for any payload to travel into space. Based on the requirements set forth by NASA documentation, this thesis establishes appropriate assembly procedures for the construction of a space payload. Detailed design changes are described, as well as any problems encountered during assembly. Various lessons learned throughout the course of this project are discussed.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.