Results 1 to 5 of about 8 (5)

Power Contingency/Margin Methodology and Operational Envelope Analysis for PlanarSats

Aerospace
This paper presents a power-centric systems-engineering approach for PlanarSats and for atto-, and femto-class spacecraft where surface-limited power dominates design.
Mehmet Şevket Uludağ, Alim Rüstem Aslan   +1 more
doaj   +2 more sources

An Analytical Framework for Determining the Minimum Size of Highly Miniaturized Satellites: PlanarSats

Aerospace
This paper introduces a power-driven systems engineering methodology for the early-phase design of highly miniaturized satellites: PlanarSats. We derive an analytical framework linking power requirements, contingency policies, solar-cell performance, and
Mehmet Şevket Uludağ, Alim Rüstem Aslan   +1 more
doaj   +2 more sources

EsTRACE—Es-Layer TRAnsient Cloud Explorer: PlanarSat Mission Concept and Early-Phase Design (Bid, CoDR, PDR) for Sporadic-E Sensing

Applied Sciences
Sporadic-E (Es) layers can strongly perturb HF/VHF propagation and create intermittent interference, motivating higher-revisit monitoring at the frequencies most affected.
Mehmet Şevket Uludağ, Alim Rüstem Aslan   +1 more
doaj   +2 more sources

Tailoring Model‐Based Systems Engineering for Sub‐100 g PlanarSats: A Power‐First View Stack

Systems Engineering
ABSTRACT This paper addresses how to apply model‐based systems engineering (MBSE) to ultrasmall planar satellites under severe power and resource constraints. PlanarSats are sub‐100‐gram spacecraft built as single printed‐circuit boards where the same surface must host both electronics and solar cells, so power generation, geometry ...
Mehmet Şevket Uludaǧ, Alim Rüstem Aslan   +1 more
openaire   +1 more source

Highly-miniaturized spacecraft “PlanarSat”: Evaluating prospects and challenges through a survey of femto & atto satellite missions

Acta Astronautica
Mehmet Şevket Uludağ, Alim Rustem Aslan   +1 more
openaire   +1 more source