FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W156770963> ?p ?o ?g. }

• W156770963 abstract "With recent technological advances, small satellite systems have evoked great interest from both commercial and military sectors. These systems offer reductions in both development time and mission cost, which make them attractive alternatives to the large systems in use today, especially for developing space nations. Small satellites are inherently less capable due to their resource constraints, yet as technology advances, a widening array of supportable missions may be enabled. Due to this, it is important for future Space Situational Awareness (SSA) applications to understand and analyze the capabilities and limitations of these small systems. In order to achieve this, a subsystem-by-subsystem analysis approach may be employed to define the capabilities of each sub-system that may be found in a small satellite. This study is intended to analyze the propulsion sub-system and define an upper bound for translational performance in micro-satellites. During the study, each element of the propulsion subsystem was characterized in terms of the satellite size to define the metrics that have the greatest effect on the overall performance. Both monopropellant and cold gas propulsion, which are proven and viable options for small satellites, were chosen for the analysis. From this study, conclusions can be drawn for both systems that identify the upper bounds of available Delta-V in terms of the sub-system and overall satellite size. APPROACH & ASSUMPTIONS Before beginning the analysis, assumptions were made to place boundaries on the satellite and system size parameters. First, the satellite size range will be constrained in order to focus the study on the “smallsat” regime. The starting point for the satellite size spectrum to be analyzed will be defined as a 10 cubic centimeter, 1 kilogram, CubeSat. Currently, CubeSat development can be found in the commercial and government sectors alike due to their promise of reduced cost and development time. Therefore, these satellites are a logical lower bound for this study due to an increased interest to use them as test-beds for new technology development and demonstration. The upper bound for satellite size has been defined as a 100centimeter cube with an estimated weight of between 100 and 150 kilograms. This will allow for analysis in the classifications of pico, nano, and microsatellites. For the entire range, the satellites will be assumed to be cube shaped as alternative geometries present more complicated considerations that may be the topic of future studies." @default.
• W156770963 created "2016-06-24" @default.
• W156770963 creator A5000428546 @default.
• W156770963 creator A5026495161 @default.
• W156770963 creator A5080535235 @default.
• W156770963 date "2010-01-01" @default.
• W156770963 modified "2023-09-27" @default.
• W156770963 title "Small Satellite Capability Analysis: A Systems Approach for Defining Translational Performance in Small Satellites" @default.
• W156770963 cites W1984213586 @default.
• W156770963 cites W2326365463 @default.
• W156770963 hasPublicationYear "2010" @default.
• W156770963 type Work @default.
• W156770963 sameAs 156770963 @default.
• W156770963 citedByCount "1" @default.
• W156770963 countsByYear W1567709632013 @default.
• W156770963 crossrefType "journal-article" @default.
• W156770963 hasAuthorship W156770963A5000428546 @default.
• W156770963 hasAuthorship W156770963A5026495161 @default.
• W156770963 hasAuthorship W156770963A5080535235 @default.
• W156770963 hasConcept C1034443 @default.
• W156770963 hasConcept C127413603 @default.
• W156770963 hasConcept C14279187 @default.
• W156770963 hasConcept C145804949 @default.
• W156770963 hasConcept C146978453 @default.
• W156770963 hasConcept C19269812 @default.
• W156770963 hasConcept C201995342 @default.
• W156770963 hasConcept C206345919 @default.
• W156770963 hasConcept C2778027091 @default.
• W156770963 hasConcept C31258907 @default.
• W156770963 hasConcept C41008148 @default.
• W156770963 hasConcept C77304879 @default.
• W156770963 hasConceptScore W156770963C1034443 @default.
• W156770963 hasConceptScore W156770963C127413603 @default.
• W156770963 hasConceptScore W156770963C14279187 @default.
• W156770963 hasConceptScore W156770963C145804949 @default.
• W156770963 hasConceptScore W156770963C146978453 @default.
• W156770963 hasConceptScore W156770963C19269812 @default.
• W156770963 hasConceptScore W156770963C201995342 @default.
• W156770963 hasConceptScore W156770963C206345919 @default.
• W156770963 hasConceptScore W156770963C2778027091 @default.
• W156770963 hasConceptScore W156770963C31258907 @default.
• W156770963 hasConceptScore W156770963C41008148 @default.
• W156770963 hasConceptScore W156770963C77304879 @default.
• W156770963 hasLocation W1567709631 @default.
• W156770963 hasOpenAccess W156770963 @default.
• W156770963 hasPrimaryLocation W1567709631 @default.
• W156770963 hasRelatedWork W110072253 @default.
• W156770963 hasRelatedWork W1588252317 @default.
• W156770963 hasRelatedWork W1974707543 @default.
• W156770963 hasRelatedWork W2065242143 @default.
• W156770963 hasRelatedWork W20778254 @default.
• W156770963 hasRelatedWork W2146818074 @default.
• W156770963 hasRelatedWork W2314870837 @default.
• W156770963 hasRelatedWork W2488697333 @default.
• W156770963 hasRelatedWork W2491213704 @default.
• W156770963 hasRelatedWork W2768051113 @default.
• W156770963 hasRelatedWork W2790764120 @default.
• W156770963 hasRelatedWork W2912107197 @default.
• W156770963 hasRelatedWork W3018912371 @default.
• W156770963 hasRelatedWork W3046022077 @default.
• W156770963 hasRelatedWork W31028464 @default.
• W156770963 hasRelatedWork W3134152645 @default.
• W156770963 hasRelatedWork W49313435 @default.
• W156770963 hasRelatedWork W627075990 @default.
• W156770963 hasRelatedWork W637689843 @default.
• W156770963 hasRelatedWork W778025099 @default.
• W156770963 isParatext "false" @default.
• W156770963 isRetracted "false" @default.
• W156770963 magId "156770963" @default.
• W156770963 workType "article" @default.