scholarly journals Seal Joint Analysis and Design for the Ares-I Upper Stage LOX Tank

Author(s):  
Dawn Phillips ◽  
Robert Wingate
2019 ◽  
Vol 974 ◽  
pp. 583-588
Author(s):  
Alexander I. Danilov

The subject of the article is to give a full analysis of the cascade type layouts in elements strengthening design in bending by gluing the fiber reinforced polymer (FRP) materials on their surfaces’ applicability and effectiveness. The research objectives are the substantiation elements cascade method application reinforcement with adhesive joints. Materials and methods are revealed in a few variants of FRP-reinforcement with application of FEM simulation. A number of diagrams and tables represent the results. The results are defined in the cost-effective efficient method presentation of the bent elements strengthening to increase their bearing capacity reserves, the features of the bonded joint behavior, the equations and formulae for the glue joint analysis and design. Conclusions are formulated in depicting the “cascade” reflects, the features of the proposed strengthening design, the base element unloading, which is gradual with each successive element attached. The design examples are oriented on the adhesive joints’ application possibility analysis of attaching the FRP elements. The results suggest the effective use possibility of the adhesive joints to strengthen rather stiff, including steel, elements in bending. The cascade method eliminates the indispensability of highly expensive high-strength materials, thereby reducing the reinforcement structures cost.


SIMULATION ◽  
2013 ◽  
Vol 89 (7) ◽  
pp. 790-809 ◽  
Author(s):  
Weilin Li ◽  
Min Luo ◽  
Lin Zhu ◽  
Antonello Monti ◽  
Ferdinanda Ponci

Author(s):  
Stephen L. Canfield ◽  
Marshall A. Norris ◽  
Seth V. Knight ◽  
Kirk F. Sorensen

Momentum eXchange Electrodynamic Reboost, or MXER, tether systems have been proposed to serve as an “upper stage in space” [1]. A MXER tether station would boost spacecraft from low Earth orbit to a high-energy orbit quickly, like a high-thrust rocket. Then, using the same principles that make an electric motor work, it would slowly rebuild its orbital momentum by pushing against the Earth’s magnetic field without using any propellant. One of the significant challenges in developing a momentum-exchange / electrodynamic reboost tether system is in the analysis and design of the capture mechanism and its effects on the overall dynamics of the system [2]. A capture mechanism that provides nearly passive operation is presented and described in [3] and led to the fabrication of a prototype article of this mechanism. This paper will describe the process of testing this prototype in a dynamically similar environment and validating an associated dynamic model. The primary contributions of this paper will be a description of the proposed capture mechanism concept and associated testing process and the validation of a dynamic model of this mechanism.


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