Missile Guidance System Bracket

Missile Guidance System Bracket ensures minimal flexural deformation under mechanical load, preserving sensor calibration baselines during dynamic flight. The bracket is machined from aerospace-grade billet stock with uniform grain orientation and post-heat treated to T6 or solution-annealed conditions. Torsional stiffness and axial loading thresholds are qualified to prevent positional drift of EO/IR and RF seeker modules under load. 

Missile Guidance System Bracket features milled or ground mounting interfaces with surface flatness and roughness controlled below 1.6 Ra µm. High surface deviation in mounting plates can cause stress concentration or angular misalignment at sensor-bracket mating zones. The bracket’s contact faces are precision-controlled to ensure uniform preload distribution and thermal path continuity with mounted guidance subsystems.