Does anyone know of an easy way to figure a required net climb gradient from SID charts? I know on the Jepp plates there are the tables that convert a required climb gradient in ft/nm to ft/min based on different aircraft groundspeeds, but a lot of turbojet aircraft performance charts only give the aircraft's net climb gradients as a percentage (i.e. Second Segment Takeoff Net Climb Gradient is found to be 1.6%). I am wondering if anyone has a shortcut method for calculating a required climb gradient from the SID charts as an expression of a certain percentage.
Thanks!
Thanks!