Generic deployable spacecraft configurations and deployable platform systems concepts were identified. Sizing, building block concepts, orbiter packaging, thermal analysis, cost analysis, and mass properties analysis as related to platform systems integration are considered. Technology needs are examined and the major criteria used in concept selection are delineated. Requirements for deployable habitat modules, tunnels, and OTV hangars are considered.
Development of Deployable Structures for Large Space Platform Systems, Volume 1
1982
185 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Astronautics , Large space structures , Space erectable structures , Space platforms , Spacecraft configurations , Structural design criteria , Systems integration , Deployment , Mechanical properties , Packaging , Payload mass ratio , Space stations , Space transportation system
Space deployable unit and large-scale deployable platform
Europäisches Patentamt | 2023
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