Abstract
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Philip B. Klocke, Emily A. Mangus, Trevor Carter, Larry L. Howell
Abstract
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Confidence 100%
openalex
Confidence 95%
No local reference links have been materialized yet.
No local citing links have been materialized yet.
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Active vibration control during deployment of space structures
10.1016/0022-460x(92)90356-3 · doi-reference
Design of a vibration isolation system for the space telescope
10.2514/1.g001221 · doi-reference
Vibration isolator for large space telescopes
10.2514/1.12036 · doi-reference
Investigation of ultra violet (UV) resistance for high strength fibers
10.1016/j.asr.2005.04.098 · doi-reference
Complete atomic oxygen and UV protection for polymer and composite materials in a low earth orbit
10.1021/acsami.0c21552 · doi-reference
Space environment and vacuum properties of spacecraft materials
10.1016/s0042-207x(81)80042-5 · doi-reference
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10.1016/0043-1648(90)90078-o · doi-reference
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10.2514/3.25761 · doi-reference
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10.3390/polym15183786 · doi-reference
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10.1115/1.4066566 · doi-reference
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10.1007/s40684-019-00027-2 · doi-reference
Design and analysis of a solid surface deployable antenna mechanism based on flasher rigid origami
10.1016/j.tws.2024.112033 · doi-reference
Deployment dynamics analysis of an origami-folded spacecraft structure with elastic hinges
10.2514/1.a34938 · doi-reference
One-DOF hexagonal thick-panel origami with uniform thickness, flat deployable surface and compact folding
10.1016/j.mechmachtheory.2025.106252 · doi-reference
A review of geometric modeling design and deployment mechanism of flasher-based origami
10.1115/1.4067717 · doi-reference