WebThe lean-, rich-burn materials test burner rig at NASA LeRC is used to evaluate the high temperature environmental durability of aerospace materials. The rig burns jet fuel and pressurized air, and sample materials can be subjected to both lean-burn and rich-burn environments. As part of NASA's Enabling Propulsion Materials (EPM) program, an … WebThe High-Flow Jet Exit Rig at the NASA Glenn Research Center is designed to test single flow jet nozzles and to measure the appropriate thrust and noise levels. The rig has been designed for the maximum hot condition of 16 lbm/sec of combustion air at 1960 R (maximum) and to produce a maximum thrust of 2000 lb.
Special Projects Laboratory Historic Documents - NASA
WebDec 1, 1999 · NASA GRC's High Pressure Burner Rig Facility and Materials Test Capabilities The High Pressure Burner Rig (HPBR) at NASA Glenn Research Center is a high-velocity. … WebDec 21, 2004 · Abstract A high-pressure burner rig was developed to evaluate the response of chemical-vapor-deposited SiC material during exposure to simulated gas turbine combustor conditions. Linear weight loss and surface recession rates of SiC were observed in both fuel-lean and fuel-rich gas mixtures. darren cook real estate
F402-RR
WebHigh pressure is achieved by the input compressed air mass flow, combustion expansion, andexhaustpressure.Theexhaustischokedbyapneu- matic Annin valve downstream of the … WebJan 1, 2024 · Product Module Rig Test. NASA Technical Reports Server (NTRS) Holdeman, James D. (Technical Monitor); Chiappetta, Louis, Jr.; Hautman, Donald J.; Ols, John T.; Padget ... WebJun 1, 2024 · High pressure burner rig testing was used to evaluate the coating system performance and durability. Test results demonstrated the feasibility and durability of the coating component systems under the simulated engine environments. Test Results for Rotordynamic Coefficients of the SSME HPOTP Turbine Interstage Seal with Two Swirl … bison rapid city