Creuziger, A.
, Chemello, C.
, Mardikian, P.
and Alexander, J.
(2024),
Metallurgical Analysis and Conservation of Turbine Blades from Recovered Apollo F-1 Engines, Studies in Conservation, [online], https://doi.org/10.1080/00393630.2024.2303891, https://tsapps.nist.gov/publication/get_pdf.cfm?pub_id=936021
(Accessed December 2, 2024)
Official websites use .gov
A .gov website belongs to an official government organization in the United States.
Secure .gov websites use HTTPS
A lock (
) or https:// means you’ve safely connected to the .gov website. Share sensitive information only on official, secure websites.
Metallurgical Analysis and Conservation of Turbine Blades from Recovered Apollo F-1 Engines
Published
Author(s)
, Claudia Chemello, Paul Mardikian, Jerrad Alexander
Abstract
Turbine blades from a recovered F-1 engine from the Apollo 16 Saturn V rocket were examined to determine an appropriate conservation protocol. Significant corrosion damage was observed in the turbine blades which appear to be made of a nickel based ' superalloy. Pitting corrosion appears to have breached the surface of the turbine blades, and subsequently a form of dealloying corrosion preferentially attacked the ' phase, leaving behind a thin network of interconnected phase. The particular alloy used for these turbine blades does not appear to be a known production alloy and may have been developed specifically for use in the F-1 rocket engines, with an increased concentration of refractory (Mo, Nb) elemental additions. The analytical results confirmed the severe loss of density of the blades and helped conservators determine a suitable treatment protocol for more than 400 blades and 100 fragments from four recovered turbines.Citation
Studies in Conservation
Pub Type
Journals
Download Paper
Citation
Issues
If you have any questions about this publication or are having problems accessing it, please contact reflib@nist.gov.
Created March 4, 2024, Updated May 10, 2024