RANCANG BANGUN AEROMODELING FIXED WING MATERIAL KOMPOSIT SANDWICH CARBON FIBER DENGAN CORE KAYU BALSA

TITO SHAFARUDIN UTOMO (2024) RANCANG BANGUN AEROMODELING FIXED WING MATERIAL KOMPOSIT SANDWICH CARBON FIBER DENGAN CORE KAYU BALSA. D3 thesis, Universitas Muhammadiyah Yogyakarta.

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Abstract

Perancangan bertujuan untuk menemukan dan menentukan bentuk dari pesawat aeromodeling fixed wing dengan material komposit sandwich yang ringan namun cukup kuat untuk memenuhi standar kendaraan udara tak berawak. Dalam manufaktur ini wingspan menggunkan material komposit sandwich yang terbuat dari kayu balsa (core) yang akan dilapisi carbon 200 gsm (skin) dengan metode vacuum bagging menggunakan resin polyester yukalac 157 BTQN. Wingspan berukuran 1600 x 200 x 20 mm. Wingspan berhasil dibuat menggunkan material komposit sandwich dengan metode vaccum bagging dengan berat 11184 g.

Item Type: Thesis (D3)
Uncontrolled Keywords: aircraft, aeromodeling, fixed wing, sandwich composite, balsa wood, carbon fiber, vaccum bagging
Divisions: Program Vokasi > D3 Teknologi Mesin
Depositing User: Aidilla Qurotianti
Date Deposited: 08 Nov 2024 03:16
Last Modified: 08 Nov 2024 03:25
URI: https://etd.umy.ac.id/id/eprint/48263

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