Master of Science (M.S.), University of Dayton, 2024, Aerospace Engineering
This research introduces an Origami-inspired dynamic spacecraft radiator,
capable of adjusting heat rejection in response to orbital variations and extreme
temperature fluctuations in lunar environments.
The research centers around the
square twist origami tessellation, an adaptable geometric structure with
significant potential for revolutionizing radiative heat control in space.
The investigative involves simulations of square twist origami tessellation panels
using vector math and algebra. This study examines both a two-dimensional (2-
D), infinitely thin tessellation, and a three-dimensional (3-D), rigidly-foldable
tessellation, each characterized by an adjustable closure or actuation angle “φ”.
Meticulously analyzed the heat loss characteristics of both the 2D and 3D
radiators over a 180-degree range of actuation.
Utilizing Monte Carlo Ray Tracing and the concept of “view factors”, the study
quantifies radiative heat loss, exploring the interplay of emitted, interrupted, and
escaped rays as the geometry adapts to various positions. This method allowed
for an in-depth understanding of the changing radiative heat loss behavior as
the tessellation actuates from fully closed to fully deployed. The findings reveal a
significant divergence between the 2D and 3D square twist origami radiators.
With an emissivity of 1, the 3D model demonstrated a slower decrease in the
ratio of escaped to emitted rays (Ψ) as the closure/actuation angle increased,
while the 2D model exhibited a more linear decline. This divergence underscores
the superior radiative heat loss control capabilities of the 2D square twist origami
geometry, offering a promising turndown ratio of 4.42, validating the model's
efficiency and practicality for radiative heat loss control.
Further exploration involved both non-rigidly and rigidly foldable radiator models.
The non-rigidly foldable geometry, initially a theoretical concept, is realized
through 3D modeling and physica (open full item for complete abstract)
Committee: Rydge Mulford (Advisor)
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