Accelerated Mechanical Testing: Profilometry-Based Indentation Plastometry (PIP) for Space & Aerospace Alloy Characterisation
Profilometry-Based Indentation Plastometry (PIP) offers an alternative methodology. Using a macroscopic indentation (50–200 µm deep), PIP captures the full indent profile and applies an accelerated inverse finite element analysis to extract a complete stress–strain curve, including yield strength and ultimate tensile strength. Applicable to a wide range of metallic materials, PIP testing provides mechanical data in under five minutes with minimal surface preparation. Furthermore, PIP can also be conducted at elevated temperatures up to 800 °C, extending its utility to high-temperature aerospace alloys.
Two recent collaborative studies with NASA demonstrate the technique’s versatility for AM component evaluation. The first investigated a laser powder bed fusion (LPBF) NASA HR-1 c-ring, mapping mechanical property variation both up the build height and across changing cross-sections. PIP revealed localised property gradients associated with thermal history and geometry-dependent cooling rates. The second study examined NASA HR-2 alloy at elevated temperatures, assessing the sensitivity of plasticity behaviour to heat treatment variations. The rapid testing capability of PIP enabled a systematic exploration of process–property relationships within hours rather than weeks.
These studies highlight PIP as a tool for accelerated, spatially resolved, and high-temperature mechanical characterisation of aerospace and space alloys, supporting the rapid qualification of next-generation AM materials.
