Publication Date:
2019-06-28
Description:
The deployment kinematics, stowing philosophy, and deployment sequencing for large deployable antenna modules were verified. Mesh attachment methods compatible with full scale modules were devised. Parametric studies of large modular reflectors established size, mass, and aperture frequency capabilities for these assemblies. Preliminary studies were made devising means of delivering modules to orbit, and once there, of assembling the modules into complete modular antenna reflectors. The basic feasibility of creating mass efficient modules erectable into large structures in space was established.
Keywords:
GROUND SUPPORT SYSTEMS AND FACILITIES (SPACE)
Type:
NASA. Marshall Space Flight Center The 15th Aerospace Mech. Symp.; p 147-157
Format:
text
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