Multiconfiguration Loads Analysis for Missions with an Uncertain Rideshare Manifest

Multiconfiguration Loads Analysis for Missions with an Uncertain Rideshare Manifest

Utah State University, Logan, UT

Rideshare or “multi-manifest” missions – where several smaller “rideshare” spacecraft are launched together, usually with a larger “forward” spacecraft – are becoming increasingly common. In many cases, the properties or configuration of the rideshare spacecraft are not well-defined during initial launch manifesting and may not be finalized until a few months before launch. In this paper, a multiconfiguration loads analysis (MLA) process is presented that can enable flexibility in the mission manifesting process by allowing for uncertainty in the final rideshare configuration, including late manifest changes or swaps, without requiring additional loads analyses to those specified in the Load Cycle Process. By applying the MLA process, a set of adequately conservative loads can be generated for the forward spacecraft, launch vehicle, and potential rideshare spacecraft that account for uncertainty in the rideshare manifest and minimize the potential for issues late in the process. The MLA process will also define a mission-specific dynamic properties envelope that would allow rideshare spacecraft that “fit” within the envelope to be swapped. If all parts of the system are verified to match the models used in analysis and designed to survive the bounding loads, the launch manifest can be changed after analyses are completed, much closer to launch, without incurring increased risk.