The ASTRO-1 preliminary design review coupled loads analysis

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National Aeronautics and Space Administration, George C. Marshall Space Flight Center, For sale by National Technical Information Service] , [Marshall Space Flight Center, Ala.], [Springfield, Va
Reusable space vehicles -- Design and construction, Materials -- Dynamic te
StatementDavid S. McGhee
SeriesNASA technical memorandum -- 82587
ContributionsGeorge C. Marshall Space Flight Center
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL14925770M

Get this from a library. The ASTRO-1 preliminary design review coupled loads analysis. [David S McGhee; George C. Marshall Space Flight Center.]. Astro-I Design Study. The upper body of the Astro-I was constructed of fiberglass, in two sections.

The front, comprised of the nose, front fenders and windshield, was fixed. A small access panel ahead of the windshield enabled access to the battery, the braking system's dual master cylinder, and the windshield washer reservoir.

A large, single. Astro-I Design Study The Astro-I was equipped with this experimental Corvair engine, with a bore and stroke of and inches, displacing cubic inches. It was air-cooled, but unlike the production engine, used three tandem centrifugal blowers on a common shaft above the engine to blow cooling air over the cylinder blocks.

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Spaceflight experience STS/Astro-1 Columbia (December 2Decem ). The Astro observatory is a unique complement of three telescopes designed to simultaneously record spectral data, polarimetric data and imagery of faint astronomical objects in the far ultraviolet.

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