Abstract: A reticle gunsight is illuminated by a chemical illumination stick which is nserted through a tapped port in a lower chamber of the gunsight. The tapped port is closed with a threaded plug to retain light within the lower chamber. The lower chamber has an optical opening therein which is aligned with reticle cross hairs to produce a light beam having the image of the cross hairs. The light beam is focussed through a collimated lens and then directed by a prism onto a beam splitter in an upper chamber of the reticle gunsight. The upper chamber is open at both ends and is aligned with the barrel of the gun so that when the image of the target is superimposed with the image of the reticle in the beam splitter, the person using the gun knows that the gun is aimed at the target. Since the gunsight does not rely on electrical illumination and does not itself illuminate the target, many deficiencies associated with previous gunsight configurations are eliminated.

Abstract: To determine the optimum load a laminate member or element is capable of bearing, a three-dimensional progressive analysis is proposed in which the stress and strain states of each ply of the laminate are subjected to failure criteria. If there is failure, new ply stiffness parameters are calculated. Thereafter, the ply is tested with the new parameter until the optimal load is determined. If no failure is detected for a given stress and strain for the ply then the load may be incremented and again applied to the ply, for further testing. Alternatively, the same load may be applied to the ply for a further period of time, until the optimal load is determined and/or the analysis is deemed to be finished.

Abstract: A method of and system for mortar fuze apex arming is disclosed in which a icroprocessor circuit is added to the M734 class of mortar proximity fuzes such that, at launch, the microprocessor measures the turbine-alternator frequency and the Doppler frequency and uses those values to calculate or look up the charge and angle used by the gunner firing the mortar as well as the time of flight to the trajectory apex, based on stored firing table or equation information. The microprocessor then causes the electrical arming of the fuze at the apex of the flight of the mortar round, using existing arming circuits already present in the M734 class of mortar proximity fuzes. Alternatively, the microprocessor may cause the electrical arming of the fuze just prior to the desired height of burst for the mortar round.