Plastic; o/a 8.5 in. dia,0.625 in. thk; furnished w/case; 1 sc ea listed sc name/sc range/sm increments grad to 360 deg/1 deg,lat/0 to 90 deg/0.5 deg,motion of body/0 to 15 min/0.1 min,polaris q factor,polaris zn correction/0 to p2.1 to 0 and 0 to m2.1 to 0 deg/0.1 deg,lat/equator to 65 deg n/5 deg,acft lat/1 to 70 deg/1 deg,coriolis correction/0.1 to 59 min/0.1 min,star relative bearing/0 to 89.5 deg/0.5 deg,motion of observer correction/1 to 9 min/0.5 min,ground speed/90 to 2000 knots/10 knots,dist/var and intercept dist/2 ea 0 to 120 miles/1 mile,0 deg lat gnc template peripheral zn/0 to 360 deg/1 deg,0 deg lat gnc template subtraction/0 deg lat jn template peripheral zn/0 to 360 deg/1 deg,0 deg lat jn template special features

A computer for the determination of two or more mavigational factors which determines the position, course and distance of an aircraft, missile, vessel or ground vehicle. Do not use if a more specific item mane applies. See also computer, altitude-azimith; computer, azimuth; computer, bomb-navigational; computer, correction; computer, course-distance; computer, flight director; computer, heading; computerm heading-track; computer, mach number; computer, magenetic variation; computer, present position; computer, range; computer, speed and latitude correction; computer, stabilization data; computer, target intercept; and computer, track.