The design, capabilities, and subsystem options for the Boeing Small Research Module (BSRM) are described. Specific scientific missions are defined based on NASA-Ames Research Center requirements and the BSRM capability to support these missions is discussed. Launch vehicle integration requirements and spacecraft operational features are also presented. (Author)
Feasibility Study of the Boeing Small Research Module (Bsrm) Concept
1975
26 pages
Report
Keine Angabe
Englisch