Thermal considerations of internal and external launch vehicle components play an important role in the development of aerospace vehicles. A system level thermal analysis provides the thermal analyst with the necessary information to ensure that designs meet the appropriate thermal requirements by aiding in the prediction of the maximum, minimum, and bulk zone temperatures that can be used for more detailed analyses.

With the vast amount of experience at ATA, we can provide you with the expertise in thermal analysis to properly characterize the system level thermodynamics of your launch vehicle, enabling you to determine thermal management requirements and perform trade studies early in the design phase.

Case Studies

• Thermal Analysis of Kistler K-1 Reusable Launch Vehicle