Designed for thermal oxidation stability testing of aviation turbine fules; 100 - 380 c test temp; 0 - 300 mm hg pressure differential; 500 psi system pressure; large lcd touch screen; rs-232 usb (2) interfaces; 115v, 8a or 230v, 4a; 47 - 63 hz; less than 600 mls needed for testing sample; pour-and-go operation; automatic aeration and fuel cleaning at beginning of testing
No other part numbers with same form, fit, and function found.
A collection of items, such as mechanical test unit, control and data acquition unit, tools and the like, primarily designed for testing and evaluating fuel lubricity, measuring boundary friction coefficient of lubricants and assessing wear by measuring the diameter of the wear scar on test ball. excluders tester, lubricant friction.
NSN 6110-01-503-1552
NSN 6135-01-431-6801
NSN 5930-01-220-1990
NSN 6130-01-400-6123
NSN 6150-01-437-7402
NSN 5998-01-061-8586
NSN 6130-01-423-0612
NSN 5996-00-572-7288
NSN 5910-01-146-2536
NSN 6220-01-231-7601
NSN 6240-00-397-3864
NSN 5855-00-832-9341