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Holddown arm release mechanism used on Saturn vehicles

Authors :
Phillips, J. D
Tolson, B. A
Source :
9th Aerospace Mech. Symp..
Publication Year :
1975
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1975.

Abstract

With the development of the Saturn launch vehicle, it became mandatory to develop a system for restraining the vehicle until after all checks and engine thrust buildup were completed. The basic Saturn I holddown arm constrains the vehicle by clamping it between a fixed support and a movable jaw. The jaw is on a link pinned to rotate sufficiently to release the vehicle. There are three links in the jaw (restraining) system arranged so that with a small force provided by a pneumatic separator mechanism, the large loads of the vehicle can be restrained. Design details discussed are the link system, the separator, adjustments, and the energy absorber. The function of preloading is discussed. The secondary release system is described. Finally, the design differences between the Saturn I and the Saturn V arm are described.

Details

Language :
English
Database :
NASA Technical Reports
Journal :
9th Aerospace Mech. Symp.
Publication Type :
Report
Accession number :
edsnas.19760012107
Document Type :
Report