06 · ENGINEERING LOG
Technical notes, architecture studies, development history, and explicit validation limits. Every article is dated when published—not backdated to make the project appear older.
An objective assessment of potential observation, mapping, and communications roles—alongside the operational, legal, weather, sensing, and humanitarian limits that could make deployment inappropriate.
The journal distinguishes project evidence from engineering inference. Hardware that has not flown is never presented as flight validated, and reconstructed history is identified as retrospective documentation.
The evidence record for Rev A Stage 6: complete digital component placement, functional zoning, sensor and power separation, unrouted connectivity retained for review, and the human mechanical gate required before controlled routing.
Read articleHow ARES-FC-REV-A-SCH-5C.0 reduced scope, closed its schematic checks, and became eligible for PCB placement consideration without claiming routing, fabrication, or flight readiness.
Read articleA reconstruction of the software problems that made the first MAVLink connection difficult to interpret, and the controls added to make connection state and command authority explicit.
Read articleA conservative concept for keeping command authority, telemetry evidence, and recovery behavior understandable when coastal communications degrade.
Read articleThe proposed antenna system combines close-range omnidirectional coverage with a future tracked directional path, while retaining manual control and clear validation gates.
Read articleA companion computer could reduce high-bandwidth dependence and enable local processing, but it adds mass, power, heat, software, cybersecurity, and integration burdens.
Read articleLower mass and simpler integration can accelerate early validation, but the aircraft becomes more dependent on communication links and the ground station.
Read articleA design study examining payload access and propulsion redundancy alongside drag, wiring, structural, and asymmetric-thrust penalties.
Read articleThe conventional layout reduces joints and manufacturing complexity but offers less room for large gimbals and modular payloads.
Read articleCenterline propulsion reduces asymmetric thrust but creates rear-propeller inflow, cooling, clearance, structure, and integration challenges.
Read articleA conceptual airframe architecture prioritizing corrosion-aware materials, protected avionics, replaceable non-critical panels, and inspectable payload interfaces.
Read articleA transparent reconstruction of how ARES ReFlight moved from project scope and software experiments toward a public site and a broader technical research agenda.
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