Navigation and Avionics
Linear accelerometers, other than those specified in 7A001, designed for use in inertial navigation systems or in guidance systems of all types, usable in ‘missiles’, having all of the following characteristics, and specially designed components therefor: a. A "bias""repeatability" of less (better) than 1 250 micro g; and b. A "scale factor""repeatability" of less (better) than 1 250 ppm;