A Predictive Model for Micrometeoroid Damage to Gossamer Structures
Michaela N. Villarreal, Jonathan W. Arenberg, and Lauren Halvonik, Harris

TL;DR
This paper develops a predictive model for micrometeoroid damage to inflatable space structures, integrating fragmentation theory, hyper-velocity testing, and gas expenditure analysis to optimize shield design and lifespan.
Contribution
It introduces a novel theoretical and empirical framework for estimating micrometeoroid damage and gas loss in gossamer space structures, enhancing damage prediction accuracy.
Findings
The model accurately predicts damage rates near 1 AU.
Shield effectiveness can be optimized based on the model.
Gas expenditure estimates inform mission lifetime planning.
Abstract
A typical inflatable reflector for space application consists of two thin membranes with a parabolic shape. It is critical to understand the interaction of the inflatable and the micrometeoroid environment to which it is exposed. This interaction leads to a series of penetrations of the inflatable membrane on entrance and exit of the impacting particle, creating a pathway for gas escape. To increase the fidelity of the damage expected, we examine the literature for descriptions of micrometeoroid fragmentation and present a theoretical formulation for the damage caused by an impacting particle to the entrance and exit membranes. This theory is compared to an initial set of hyper-velocity tests for micrometeoroid-sized particles on thin film membranes. We use the results of these tests to produce a predictive model. This model is applied to estimate the damage rate near the 1 AU location…
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Taxonomy
TopicsSpacecraft Design and Technology · Space Satellite Systems and Control · Silicone and Siloxane Chemistry
