Relevant bibliographies by topics / Deployable boom

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Deployable boom'

Author: Grafiati
Published: 4 June 2021
Last updated: 28 January 2023

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Journal articles on the topic "Deployable boom"

1

Iuvshin, A. M., Y. S. Andreev, and S. D. Tretyakov. "Development of Forming Method of Deployable Boom from Thermoplastic Polymer Composite." Key Engineering Materials 887 (May 2021): 105–9. http://dx.doi.org/10.4028/www.scientific.net/kem.887.105.

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This paper studies deployable elements which are used in satellites and different terrestrial antenna devices. Many deployable elements are made from steel or thermoset polymer composite materials and have the following disadvantages like length limitation of deployable elements, labour intensity of manufacturing process of deployable elements etc. For this purpose a deployable tube boom element was chosen and a forming method for manufacturing deployable tube element from thermoplastic polymer composite material was developed.
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Yang, Hui, Shuoshuo Fan, Yan Wang, and Chuang Shi. "Novel Four-Cell Lenticular Honeycomb Deployable Boom with Enhanced Stiffness." Materials 15, no. 1 (2022): 306. http://dx.doi.org/10.3390/ma15010306.

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Composite thin-walled booms can easily be folded and self-deployed by releasing stored strain energy. Thus, such booms can be used to deploy antennas, solar sails, and optical telescopes. In the present work, a new four-cell lenticular honeycomb deployable (FLHD) boom is proposed, and the relevant parameters are optimized. Coiling dynamics analysis of the FLHD boom under a pure bending load is performed using nonlinear explicit dynamics analysis, and the coiling simulation is divided into three consecutive steps, namely, the flattening step, the holding step, and the hub coiling step. An optim
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Chen, Manming, Zonghao Pan, Tielong Zhang, et al. "Deployable boom for Mars Orbiter Magnetometer onboard Tianwen-1." JUSTC 52, no. 5 (2022): 7. http://dx.doi.org/10.52396/justc-2022-0001.

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A more than 3 m-long deployable boom is an essential component of the Mars Orbiter Magnetometer (MOMAG) onboard the orbiter of Tianwen-1. The boom was developed to place fluxgate magnetometer (FGM) sensors away from the satellite to reduce the influence of the satellite magnetic field. It was designed as an articulated spring-driven deployable mechanism for single-shot deployment. Functionality, reliability and system constraints are fully considered in the boom design. Mechanical analyses and proof tests show that the boom has sufficient safety margin to withstand environmental conditions, ev
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Chen, Manming, Zonghao Pan, Tielong Zhang, et al. "Deployable boom for Mars Orbiter Magnetometer onboard “Tianwen-1”." JUSTC 52, no. 3 (2022): 1. http://dx.doi.org/10.52396/justc-2021-0001.

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A more than 3-m long deployable boom is an essential component of the Mars Orbiter Magnetometer (MOMAG) onboard the orbiter of “Tianwen-1”. The boom was developed to place fluxgate magnetometer (FGM) sensors away from the satellite to reduce the influence of the satellite magnetic field. It was designed as an articulated spring-driven deployable mechanism for single-shot deployment. Functionality, reliability and system constraints are fully considered in the boom design. Mechanical analyses and proof tests show that the boom has sufficient safety margin to withstand environmental conditions,
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Silver, Mark J., Lee D. Peterson, and Lisa M. R. Hardaway. "Experimental Measurement of Picometer Scale Spontaneous Vibrations in a Precision Deployable Boom under Thermal Loading." Shock and Vibration 14, no. 2 (2007): 133–49. http://dx.doi.org/10.1155/2007/393578.

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This paper reports observations and analysis of picometer scale spontaneous vibrations in a precision deployable boom under thermal loading. The structural test article is a deployable boom previously flown in space. It exhibited spontaneous vibrations during the temperature rise following a night to day transition on orbit. In an attempt to reproduce the spontaneous vibrations on the ground, the test article was thermally loaded within a mechanically stabilized test environment. Spontaneous vibrations were induced in these ground experiments. The vibrations were at a scale of motion for which
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Soykasap, Ömer. "Deployment analysis of a self-deployable composite boom." Composite Structures 89, no. 3 (2009): 374–81. http://dx.doi.org/10.1016/j.compstruct.2008.08.012.

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Bai, Jiang-Bo, Di Chen, Jun-Jiang Xiong, and R. Ajit Shenoi. "Folding analysis for thin-walled deployable composite boom." Acta Astronautica 159 (June 2019): 622–36. http://dx.doi.org/10.1016/j.actaastro.2019.02.014.

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Kim, Sang Ki, and Jae Young Kang. "Deployable Carbon-Fiber-Reinforced Polymer Boom with Bi-stability." Transactions of the Korean Society of Mechanical Engineers - A 45, no. 6 (2021): 465–71. http://dx.doi.org/10.3795/ksme-a.2021.45.6.465.

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Chu, ZhongYi, and YiAn Lei. "Design theory and dynamic analysis of a deployable boom." Mechanism and Machine Theory 71 (January 2014): 126–41. http://dx.doi.org/10.1016/j.mechmachtheory.2013.09.009.

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Roh, Jin-Ho, and Jae-Sung Bae. "Softenable composite boom for reconfigurable and self-deployable structures." Mechanics of Advanced Materials and Structures 24, no. 8 (2016): 698–711. http://dx.doi.org/10.1080/15376494.2016.1196776.

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Dissertations / Theses on the topic "Deployable boom"

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Shepenkov, Valeriy. "Vibration Modal Analysis of a Deployable Boom Integrated to a CubeSat." Thesis, KTH, Strukturmekanik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-122076.

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CubeSat or Cubic Satellite is an effective method to study the space aroundthe Earth thanks to its low cost, easy maintenance and short lead time. However, a great challenge of small satellites lies in achieving technicaland scientific requirements during the design stage. In the present workprimary focus is given to dynamic characterization of the deployable tapespringboom in order to verify and study the boom deployment dynamiceffects on the satellite. The deployed boom dynamic characteristics werestudied through simulations and experimental testing. The gravity offloadingsystem was used to
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Herlem, Florian. "Modelling and Manufacturing of a Composite Bi-Stable Boom for Small Satellites." Thesis, KTH, Mekanik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-168323.

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Thin cylindrical shell structures may provide an interesting breakthrough for deployable  structures for small satellites. Its bi-stable behaviour allows two different stable configurations: coiled and deployed. Several projects worldwide are using tape springs for satellites and for the SEAM project, at KTH, 1 meter long tape springs will be used for booms. This thesis investigates the energy stored inside the tape spring according to its layup configuration and the different fiber orientations. With a thickness around 0.3 mm and a length of one meter, the booms will deploy sensors with a qui
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Mallol, Parera Pau. "Deployment Simulations of a Composite Boom for Small Satellites." Licentiate thesis, KTH, Strukturmekanik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-121633.

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The use of small satellites is rapidly growing, especially satellites with masses between 1 and 10 kg and few litres of volume. The main reasons are due to the low development time and cost. Electronics miniaturization and high density integration is enabling the small satellites class to perform more and better tasks and at a lower cost. When deployable structures are required for the missions, the actual paradigm is that there are very few that have been successfully developed and flown. It is usually not possible to scale down existing deployable structures from larger satellites. Power and
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Mao, Huina. "Numerical and Experimental Studies of Deployment Dynamics of Space Webs and CubeSat Booms." Doctoral thesis, KTH, Farkost och flyg, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-206594.

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In this thesis, experiments and simulations are performed to study the deployment dynamics of space webs and space booms, focusing on the deployment and stabilization phases of the space web and the behavior of the bi-stable tape spring booms after long-term stowage. The space web, Suaineadh, was launched onboard the sounding rocket REXUS-12 from the Swedish launch base Esrange in Kiruna on 19 March 2012. It served as a technology demonstrator for a space web. A reaction wheel was used to actively control the deployment and stabilization states of the 2×2 m2 space web. After ejection from the
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Hoskin, Adam. "Blossoming of coiled deployable booms." Thesis, University of Surrey, 2018. http://epubs.surrey.ac.uk/846077/.

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Coiled deployable booms have been used extensively in space and are a large part of the deployable space structures family. They have a wide variety of uses such as the deployment of instruments, gravity-gradient stabilisation masses and more recently solar sails. Most deployable booms are similar to a carpenter's tape measure in the way they are coiled in a retracted condition and then deploy to form the boom structure. There have been many developments in the optimisation of boom properties in the deployed state, by using different shape cross sections and by using different materials. The �
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Mallikarachchi, H. M. Yasitha Chinthaka. "Thin-walled composite deployable booms with tape-spring hinges." Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/239395.

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Deployable structures made from ultra-thin composite materials can be folded elastically and are able to self-deploy by releasing the stored strain energy. Their lightness, low cost due to smaller number of components, and friction insensitive behaviour are key attractions for space applications. This dissertation presents a design methodology for lightweight composite booms with multiple tape-spring hinges. The whole process of folding and deployment of the tape-spring hinges under both quasi-static and dynamic loading has been captured in detail through finite element simulations, starting f
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Books on the topic "Deployable boom"

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Baumeister, Joseph F. Comparative thermal analysis of the space station Freedom Photovoltaic Deployable Boom structure using TRASYS, NEVADA, and SINDA programs. National Aeronautics and Space Administration, 1989.

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Cruse, Thomas. Stiffening of deployable space booms: Automated protein crystal growth facility. Vanderbilt University, Dept. of Mechanical Engineering, 1993.

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L, Heard Walter, and Langley Research Center, eds. Packaging, deployment, and panel design concepts for a truss-stiffened 7-panel precision deployable reflector with feed boom. National Aeronautics and Space Administration, Langley Research Center, 1993.

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Book chapters on the topic "Deployable boom"

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Straubel, Marco, and Michael Sinapius. "Boom Concept for Gossamer Deployable Space Structures." In Adaptive, tolerant and efficient composite structures. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-29190-6_18.

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Szyszkowski, W., and K. Fielden. "Controlling the Performance and the Deployment Parameters of a Self-Locking Satellite Boom." In IUTAM-IASS Symposium on Deployable Structures: Theory and Applications. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-015-9514-8_42.

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Zhao, Chong, Hongwei Guo, Rongqiang Liu, Zongquan Deng, and Bing Li. "Design and analysis of a cable-driven multistage orderly deployable/retractable space telescopic boom." In Advances in Mechanism and Machine Science. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-20131-9_227.

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Conference papers on the topic "Deployable boom"

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Yang, Bingen, Hongli Ding, Houfei Fang, and Michael Lou. "Modeling and Vibration Analysis of Deployable Space Boom Structures." In ASME 2005 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/detc2005-84519.

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Lightweight booms are being developed as a basic building element of deployable space structures for future NASA missions. This paper presents an analytical modeling and solution technique, namely the Distributed Transfer Function Method (DTFM), for synthesis and design of deployable boom structures. A space boom structure in consideration is modeled as a space frame that is enhanced by springs. In the DTFM, the distributed transfer functions describing the bending, torsion, and longitudinal deformations of frame members are first derived. A global dynamic equilibrium equation of the boom stru
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Leipold, M., and A. Daton-Lovett. "Highly compact deployable and retrievable boom." In 57th International Astronautical Congress. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.iac-06-c2.2.03.

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Brown, Michael. "Recent Developments in Superstring Deployable Truss Boom." In 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
14th AIAA/ASME/AHS Adaptive Structures Conference
7th. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-1807.

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Ng, Tang-Tat, and Thomas Murphey. "A Novel Deployable Boom with Flexible Hinges." In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-2197.

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Lou, Michael C., Houfei Fang, Ben Yang, and Nathaniel Lee Palmer. "Development of an Innovative Space Boom." In ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/de-23239.

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Abstract This paper presents the development of a new type of ultra-lightweight space boom, called the Self-deployable Spring Strip Boom or simply the S3 Boom. It describes the fundamental design concept and several variations of design configurations. Test results of proof-of-concept models are discussed and compared with results obtained by analytical simulations.
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Fulton, JoAnna, Sungeun K. Jeon, and Thomas W. Murphey. "Flight Qualification Testing of a Meter-class CubeSat Deployable Boom." In 4th AIAA Spacecraft Structures Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-0621.

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Roybal, Francisco, Jeremy Banik, and Thomas Murphey. "Development of an Elastically Deployable Boom for Tensioned Planar Structures." In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1838.

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Ulliac, Andre, Katelyn Ball, Jari Swanson, Michael Lipsett, Dan Sameoto, and Ian Mann. "Optimizing Deployable Boom Designs For Stable Operation Of Nano-Satellites." In Canadian Society for Mechanical Engineering International Congress (2021 : Charlottetown, PE). University of Prince Edward Island. Robertson Library, 2021. http://dx.doi.org/10.32393/csme.2021.181.

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Herath, Madhubhashitha, Mainul Islam, Jayantha Epaarachchi, Fenghua Zhang, and Jinsong Leng. "4D Printed Shape Memory Polymer Composite Structures for Deployable Small Spacecrafts." In ASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/smasis2019-5583.

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Abstract Four dimensional (4D) printing is the convergence of three dimensional (3D) printing, which is an emerging additive manufacturing technology for smart materials. 4D printing is referred to the capability of changing the shape, property, or functionality of a 3D printed structure under a particular external stimulus. This paper presents the structural performance, shape memory behavior and photothermal effect of 4D printed pristine shape memory polymer (SMP) and it’s composite (SMPC) with multi-walled carbon nanotubes (MWCNTs). Both materials have demonstrated the ability to retain a t
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Zhang, Jun, Aiguo Song, Xiaonong Xu, and Wei Lu. "A rigid and flexible structures combined deployable boom for space exploration." In 2016 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS). IEEE, 2016. http://dx.doi.org/10.1109/iros.2016.7759452.

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