Equivalent Analysis of Thermo-Dynamic Blow-Off Impulse under X-ray Irradiation

X-ray thermodynamic effect is an important damage mode for spacecraft. Blow-off impulse as the main thermodynamic damage parameter has been widely studied by combining laboratory and numerical simulations. In this paper, most calculations and analyses have been carried out by using the self-developed software RAMA, including the equivalent calculation of blow-off impulse of monoenergetic and blackbody X-ray, and soft/hard blackbody X-ray irradiated at different incidence angles of LY-12 aluminium target. The results show that the characteristic mono-energetic X-ray can be exploited to simulate the blow-off impulse of the blackbody X-ray under certain conditions as a feasible equivalent method for the equal-flux and equal-impulse relations between mono-energetic and intense pulse blackbody of blow-off impulse. Moreover, the equivalent thermodynamic effect can be achieved between the point source radiation and parallel X-ray of X-ray. Furthermore, the cosine distribution of blow-off impulse is conducive to designing and calculating X-ray radiation load of hard aluminium corresponding to 1–5 keV blackbody spectrum. The mentioned results can be referenced for pulse X-ray simulation source and enhance the fidelity of the thermal-mechanical effect by electron beam. It is noteworthy that the study on the thermodynamic effects of intense pulsed X-ray is of high significance.

Development and Evaluation of Small Shaped Charge Jet Threats

Because of their prolific nature on the battlefield, rocket propelled and gun-launched grenades are of particular concern to the soldier, particularly because of the severe reaction that occurs when a munition is hit by the shaped charge jet. As a result of the danger that such a detonation poses, it is necessary to more precisely understand the behaviour of munitions subjected to these types of devices. In response to these threats, standardized 81 mm and 40 mm shaped charge warheads were developed for use during threat assessment testing to act as a consistent, lower-cost representative of shaped charge projectiles commonly encountered on the battlefield, and to help quantify the interaction of these jest with explosive charges. The international standards for shaped charge jet threat testing uses the Held initiation criteria V2D, where V is the jet velocity and D is the diameter. V2D was computationally predicted using the high-rate continuum models CALE and ALE-3D. The surrogate warheads were test fired through aluminium target plates to strip off jet mass to adjust the V2D to the threat munition.

Piezoelectric Properties of Sputtered AlN Thin Films and their Applications

In this study, aluminum nitride (AlN) thin films reactively sputter deposited from an aluminium target are characterized both under material related aspects as well as on device level for resonantly driven gyroscopes. The first topic comprises a qualitative evaluation of the c-axis orientation by applying a wet chemical etching procedure in phosphoric acid to specimens synthesized under varying sputter deposition conditions. Samples with a high c-axis orientation show a low etch rate and smooth surface characteristics on the etched areas and vice versa. Furthermore, a quantitative determination of the piezoelectric coefficients is presented including the impact of the silicon substrate on the change in AlN film thickness under excitation. With this advanced approach, the d33 and the d31 coefficients are gained simultaneously with high accuracy comparing FEM simulations and interferometric measurements. Finally, AlN are applied to bulkmicromachined gyroscopes to stimulate the drive mode. Parasitic effects on the performance generated by the microactuator elements are identified and potential improvements are proposed.