Experimental Testing and Maintenance of the Gas Turbine Test Facility.
Abstract
The test operation of the TCS-560 gas turbine-compressor in a closed cycle nitrogen loop is described. The design and modification of the t-c set to improve aerodynamic performance are reviewed and the results of evaluation testing following modification are presented. The general performance of test facility equipment is summarized. (Author Modified Abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1963
- Accession Number
- AD0758333
Entities
Organizations
- Aerojet Rocketdyne Holdings