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 5965-01-181-7831
NSN 6240-00-104-4662
NSN 5895-01-500-2304
NSN 6320-00-578-6898
NSN 7035-01-121-0901
NSN 5910-01-092-9399
NSN 5985-01-496-7484
NSN 5835-00-939-7470
NSN 5945-01-165-5406
NSN 5835-00-752-6065
NSN 6645-01-370-5264
NSN 5855-00-055-1579