Published Paper Details:

The SLS Launch vehicle with Orion spacecraft is going to be used for NASA's Artemis project to send humans back to the moon's first after 1972. It has been observed that during the journey to orbit, the spacecraft undergoes various payload conditions. The outer body of the nose cone and the connecting compartment have to undergo temperature changes with respect to speed, atmospheric, and pressure conditions. Due to such conditions, the spacecraft can have a serious impact on the outer surface of the nose cone. When the system is directly integrated with the Abort origin or payload fairing in both versions of SLS, it is going to have an impact. To avoid the impact and to standardize the deformation on the spacecraft, there have been changes in the design, and a modified design is compared with the current existing SLS models. This paper also reveals the study results of the simulation analysis of the nose cone of the SLS model, which have carried out simulations of the pre-existing materials, such as metals and alloys, and a new composite material is taken as a review for the analysis under the harsh and extreme conditions faced by the spacecraft and launch vehicle during the launch sequence, in space, and atmospheric re-entry. Comparing the results to get an efficient material outcome that makes the design robust, sturdy, and efficient, considering safety parameters.