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Materials, Structures and Manufacturing: An Integrated Approach to Develop Expandable Structures
Membrane dominated space structures are lightweight and package efficiently for launch; however, they must be expanded (deployed) in-orbit to achieve the desired geometry. These expandable structural systems include solar sails, solar power arrays, antennas, and numerous other large aperture devices that are used to collect, reflect and/or transmit electromagnetic radiation. In this work, an integrated approach to development of thin-film damage tolerant membranes is explored using advanced manufacturing. Bio-inspired hierarchical structures were printed on films using additive manufacturing to achieve improved tear resistance and to facilitate membrane deployment. High precision, robust expandable structures can be realized using materials that are both space durable and processable using additive manufacturing. Test results show this initial work produced higher tear resistance than neat film of equivalent mass. Future research and development opportunities for expandable structural systems designed using an integrated approach to structural design, manufacturing, and materials selection are discussed.
Some design considerations for spin-stabilized satellites with rigid expandable structures
Design considerations for spin stabilized satellites with rigid expandable structures
A CONTRIBUTION TO THE THEORY OF FOLDING DEFORMATIONS IN EXPANDABLE STRUCTURES WITH A PARTICULAR APPLICATION TO TOROIDAL SHELLS
Theory of folding deformations in expandable structures, toroidal shells
THE USE OF RADIATION INDUCED PLASTIC MEMORY TO DEVELOP NEW SPACE EXPANDABLE STRUCTURES.
Radiation induced plastic memory to develop new space expandable structures
Expandable structures technology for manned space applications
Full scale models, nonflammable materials and tests for manned space expandable structures including airlocks, transfer tunnels, station modules, lunar shelters and flexible windows
Intelligent Flexible Materials for Space Structures: Expandable Habitat Engineering Development Unit
Expandable habitable elements are an enabling technology for human exploration in space and on planetary surfaces. Large geometries can be deployed from a small launch volume, allowing greater mission capability while reducing mass and improving robustness over traditional rigid shells. This report describes research performed by ILC Dover under the Intelligent Flexible Materials for Space Structures program on the design and manufacture of softgoods for LaRC's Expandable Habitat Engineering Development Unit (EDU). The EDU is a full-scale structural test article of an expandable hybrid habitat, integrating an expandable softgoods center section with two rigid end caps. The design of the bladder, restraint layer and a mock-up Thermal Micrometeoroid Cover is detailed together with the design of the interface hardware used to attach them to the end caps. The integration and design of two windows and a floor are also covered. Analysis was performed to study the effects of the open weave design, and to determine the correct webbing and fabric configuration. Stress analyses were also carried out on the interfaces between the softgoods and the end caps and windows. Testing experimentally determined the strength of the fabric and straps, and component testing was used to proof several critical parts of the design. This program established new manufacturing and design techniques that can be applied to future applications in expandable structures.
ANALYSIS OF FOLDABILITY IN EXPANDABLE STRUCTURES
Presentation of outlines for a general theory of large, deformations including folding of arbitrary inextensible membranes
Custom Turnkey Time and Frequency Systems: A structured, expandable approach
Radiocode Clocks Ltd. have developed a Turnkey Time and Frequency Generation and Distribution, System strategy based upon a bus of three, 'core' signals from which any Time code, Pulse rate or Frequency can be produced. The heart of the system is a ruggedized 19 inch, 3U Single Eurocard chassis constructed from machined 10mm aluminum alloy plate and designed to meet stringent Military, Security and Telecommunications specifications. The chassis is fitted with an advanced multilayer backplane with separate ground planes for analog and digital signals ensuring no degradation of low noise frequency references in the proximity of high speed digital pulse transmissions. The system has been designed to be used in three possible configurations: 1) As a stand alone generation and distribution instrument; 2) As a primary distribution unit in a turnkey Time and Frequency system; and 3) As a secondary distribution unit at a remote location from the Turnkey Time and Frequency System providing regeneration of core signals and correction for transmission delays. When configured as a secondary distribution unit the system will continue to provide usable outputs when one, two or even all three of the 'core' signals are lost. The instrument's placement within a system as a possible single point of system failure has required the development of very high reliability translator, synthesizer, phase locked loop and distribution modules together with a comprehensive alarm and monitoring strategy.
Future Applications of Lightweight Expandable Structures for NASA Space Science
No abstract available
Modular Damage Detection for Expandable Structures
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Advanced structural geometry studies. Part 2: A geometric transformation concept for expanding rigid structures
Development of expandable structures concepts for application to structures used in space missions - Part 2
Development and evaluation of the elastic recovery concept for expandable space structures
Elastic recovery of expandable space structures
Mechanical properties of composite materials for expandable space structures
Mechanical properties of composite materials for expandable space structures
Materials technology advancement program for expandable manned space structures Summary report
Composite materials testing for fire resistant wall structures for expandable manned space structures
Development of an expanded core structural panel for spacecraft interior applications, part 1
A description of the estimated costs, required materials, and fabrication techniques required to produce expanded core sandwich structural panels for use in the interior of spacecraft was given.