Export restricted (ITAR), sale only to US Citizens and Organizations. Guided Missile Accelerometer Assembly made by Autonetics, a division of North American Aviation, measuring 11″ x 4.25″ x 8″, housed in its original Autnetics fiberglass case with two parts labels, “Accelerometer Assembly, Guided Missile, MX-3885 / DJW-15, Stk No. 1420-819-8046, Ser. No. AAM0718, Pt. No. 25170-102, Contr. No. AF04 (694)-224” and “Accelerometer Unit, Angular - Interstage, Part No. 50950-507, Ser. No. DED0753,” with the back stamped “7805-520516, AF04-694-224, T000544, Mar 9, 1964.” In fine condition, with scattered scuffs and marks.
Developed by Autonetics, a division of North American Aviation, which later became a part of Rockwell International, the Guided Missile Accelerometer Assembly played a crucial role in missile guidance and control systems, as it was responsible for measuring the acceleration forces acting upon the missile during flight. By accurately measuring these accelerations, the missile's guidance system could calculate its current velocity, position, and trajectory. This information was vital for ensuring that the missile stayed on its intended course, corrected its path if necessary, and ultimately hit its target with precision.
The Guided Missile Accelerometer Assembly helped provide the missile's guidance system with real-time data about its acceleration and movement, enabling the missile to make necessary adjustments to maintain its intended flight path and increase its chances of successfully reaching its designated target. This technology was a fundamental part of the evolution of guided missile systems, improving their accuracy and effectiveness in various military and defense applications.
From The Peter Gerry Collection.
