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Heliogyro Preliminary Design, Phase 2There are 12 blades in the Heliogyro design, and each blade is envisioned to be 8 meters in width and 7,500 meters in length. The blades are expected to be composed primarily of a thin membrane constructed of material such as Kapton film with an aluminum reflective coating on one side and an infrared emissive coating on the other. The present Phase 2 Final Report covers work done on the following six topics: (1) Design and analysis of a stowable circular lattice batten for the Heliogyro blade. (2) Design and analysis of a biaxially tensioned blade panel. (3) Definition of a research program for micrometeoroid damage to tendons. (4) A conceptual design for a flight test model of the Heliogyro. (5) Definition of modifications to the NASTRAN computer program required to provide improved analysis of the Heliogyro. (6) A User's Manual covering applications of NASTRAN to the Heliogyro.
Document ID
19780016313
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
January 19, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-157128
MS404-5
Accession Number
78N24256
Funding Number(s)
CONTRACT_GRANT: JPL-954709
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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