ASTROBOTIC TECHNOLOGY INC — National Aeronautics and Space Administration SBIR Phase I: Z7

Description

Astrobotic proposes the development of ldquo;Floatinator,rdquo; a one-of-its-kind tunable lunar and planetary gravity simulator for terrestrial testing of plume-surface interactions (PSI) and cratering. In its initial lunar configuration, Floatinator will consist of a hot-fire test chamber capable of being dropped at a controlled acceleration of 5/6g, thereby providing a 1/6g gravity reference frame inside the chamber. Floatinator will be outfitted with a box of regolith simulant and integrated with Astrobotic#39;s Dropinator dynamic test stand to test plume-surface interactions and deep cratering effects under the relevant gravitational conditions.nbsp;By providing a relevant lunar gravity environment, Floatinator will control for and eliminate a major variable ndash; namely, Earth gravity ndash; that has limited the applicability of all ground-based lunar PSI and cratering testing to date. This novel test platform will enable the collection of valuable data aboutnbsp;how lunar lander dust plumes will affect lander systems, onboard payloads, landing sites, and nearby surface infrastructure on upcoming CLPS, Artemis, and commercial missions. Astrobotic further proposes to expand upon this proposed scope of work in Phase II, during which it intends to conduct hot-fire engine testing in this simulated gravity environment.