Haynes 242 Alloy for Lares 2 Satellite | Zendy

D. Pilone | Zendy; A. Brotzu | Zendy; F. Felli | Zendy; Ignazio Ciufolini | Zendy; Barbara Negri | Zendy; Claudio Paris | Zendy

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Haynes 242 Alloy for Lares 2 Satellite

Author(s) -

D. Pilone,

A. Brotzu,

F. Felli,

Ignazio Ciufolini,

Barbara Negri,

Claudio Paris

Publication year - 2021

Publication title -

frattura ed integrità strutturale

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.368

H-Index - 19

ISSN - 1971-8993

DOI - 10.3221/igf-esis.56.04

Subject(s) - alloy , geodetic datum , satellite , machinability , spacecraft , shore durometer , frame (networking) , inertial frame of reference , materials science , ductility (earth science) , tensile testing , ultimate tensile strength , metallurgy , geology , mechanical engineering , engineering , aerospace engineering , geodesy , physics , creep , machining , quantum mechanics

The satellite LARES 2 is designed to test dragging of inertial frames, or frame-dragging, predicted by Einstein’s theory of General Relativity, with accuracy of a few parts in a thousand. For this purpose, besides the typical requirements for a space construction, a high density alloy must be used. In this paper are reported the studies performed on a nickel alloy, the Haynes 242, that is considered a possible candidate for manufacturing all the metallic parts of LARES 2 and other passive geodetic satellites. Haynes 242 density and mechanical properties are compliant with the requirements of the mission. Three different casting with the nominal composition of the alloy have been prepared and tested along with a commercial bar of Haynes 242. The results of tensile and hardness tests on several specimens with different aging time are reported, along with the relevant metallographic analysis. Furthermore, a test on the machinability, performed on a screw, which is the most demanding item from the manufacturing point of view, is reported.

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