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Manufacturing Research in Support of Saturn VResearch achievements applicable to the production of Saturn V components a r e described in this report.

Leakage at the mechanical connections in high-pressure lines has been minimized or eliminated through the use of precisely flared tubes. Flaring to close tolerance is done with a n orbital flaring adapter, and the forming operation is precisely controlled with an electronic control console.

A technique of “aging” or heat-treatment hardening of aluminum materials has been used to form cylindrical-tank segments and double-contoured gore segments precisely, and to remove weld distortions).


The control of weld porosity has been improved as a result of research which demonstrated the close correlation between electrical energy input per inch of weld and weld porosity and metallurgical quality. Based on this information, the gas metallic arc method has been used successfully for two-pass welding, and thinner gage aluminum has been welded (LOX tunnel to fuel bulkhead) with an MSFC designed gas metallic arc unit.
Document ID
19660027131
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Contribution to larger work
Authors
James R Williams
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Publication Information
Publication: Manufacturing Research at MSFC Research Achievements Review Series No. 8
Publisher: National Aeronautics and Space Administration
Subject Category
Space Vehicles
Report/Patent Number
NASA/TM-X-53505
Accession Number
66N36421
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPOSITE MATERIAL
WELDING
CHEMICAL MILLING
SATURN V LAUNCH VEHICLE
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