Evaluation of control parameters for Spray-In-Air (SIA) aqueous cleaning for shuttle RSRM hardware
- Author:
- Davis, S. J.
- Published:
- Mar 1, 1995.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Deweese, C. D.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary:
- HD-2 grease is deliberately applied to Shuttle Redesigned Solid Rocket Motor (RSRM) D6AC steel hardware parts as a temporary protective coating for storage and shipping. This HD-2 grease is the most common form of surface contamination on RSRM hardware and must be removed prior to subsequent surface treatment. Failure to achieve an acceptable level of cleanliness (HD-2 calcium grease removal) is a common cause of defect incidence. Common failures from ineffective cleaning include poor adhesion of surface coatings, reduced bond performance of structural adhesives, and failure to pass cleanliness inspection standards. The RSRM hardware is currently cleaned and refurbished using methyl chloroform (1,1,1-trichloroethane). This chlorinated solvent is mandated for elimination due to its ozone depleting characteristics. This report describes an experimental study of an aqueous cleaning system (which uses Brulin 815 GD) as a replacement for methyl chloroform. Evaluation of process control parameters for this cleaner are discussed as well as cleaning mechanisms for a spray-in-air process.
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19950025373.
Accession ID: 95N31794.
Aerospace Environmental Technology Conference; p 481-490. - Terms of Use and Reproduction:
- No Copyright.
- Online Version:
- hdl.handle.net
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