Abstract: Techniques for vehicle design and manufacture are described. These techniques include receiving data relating to one or more desired stiffness characteristics for a manufactured component and identifying a plurality of cross-sectional cuts for a model relating to the component. The techniques further include determining one or more material properties for the manufactured component, the one or more material properties estimated to meet the one or more desired stiffness characteristics for the manufactured component. This includes: for each cross-sectional cut, of the plurality of cross-sectional cuts: determining at least one of the one or more material properties based on identifying a potential solution to a nonlinear optimization problem using one or more initial estimates based on the desired stiffness characteristics.

Abstract: A method of collecting measurements for estimating one or more air data parameters of an aerospace vehicle is disclosed. The method includes converting, by an array of optical sensors, incident light into an optical signal indicating a measurement for estimating the one or more air data parameters. The array of optical sensors is disposed along a skin of the aerospace vehicle. The method includes measuring, by an interrogator, a wavelength of a combined optical signal, wherein the combined optical signal is a combination of the optical signals generated by each of the optical sensors that are part of the array. The method further includes converting, by the interrogator, the wavelength of the optical signal into an electronic signal indicating either the measurement for estimating the one or more air data parameters. Finally, the method includes sending the electronic signal indicating the measurement to a platform network.

Abstract: A method of collecting measurements for estimating one or more air data parameters of an aerospace vehicle is disclosed. The method includes converting, by an array of optical sensors, incident light into an optical signal indicating a measurement for estimating the one or more air data parameters. The array of optical sensors is disposed along a skin of the aerospace vehicle. The method includes measuring, by an interrogator, a wavelength of a combined optical signal, wherein the combined optical signal is a combination of the optical signals generated by each of the optical sensors that are part of the array. The method further includes converting, by the interrogator, the wavelength of the optical signal into an electronic signal indicating either the measurement for estimating the one or more air data parameters. Finally, the method includes sending the electronic signal indicating the measurement to a platform network.

Abstract: Means for mounting an engine to an aircraft are provided which reduce the dynamic response of the airframe due to engine vibration. A mount comprises at least one strut extending between the engine and the airframe which is attached to the airframe by means of damping elements.