Physics
Characterise force margins, stability, pressure, thermal and corrosion limits.
System anatomy · 05
Match lift, buoyancy, drag, pressure, corrosion, energy and payload to the intended mission conditions.
FUURAA thesis
Engineering map
Each layer states the boundary to establish and the evidence needed for the next decision.
Characterise force margins, stability, pressure, thermal and corrosion limits.
Measure mission energy with payload, current, wind, reserve and ageing included.
Verify mass, balance, hydrodynamic or aerodynamic effects and safe release.
Verification questions
Each question needs an object, conditions, denominator, threshold and accountable decision owner.
What is the tested environmental envelope?
Which condition consumes the reserve first?
How does payload change stability and recovery?
What degrades between maintenance intervals?
Evidence to preserve
A conclusion alone loses reviewability; raw records, configuration and exclusions matter too.
Environmental qualification matrix
Loaded endurance and reserve results
Inspection, corrosion and pressure records
Scope boundary
Nominal endurance or depth ratings do not establish safe mission margins in combined conditions.
This is an engineering reading and decision framework; it does not replace application-specific risk assessment, conformity work, procurement acceptance or professional advice.
Sources and evidence status
Source dates and review status remain visible; external sources open in a new tab.
Specifies requirements for safe commercial UAS operations, including external safety-critical command-and-control services.
Describes untethered AUVs executing planned missions, storing payload data, surfacing for communications and requiring later recovery and processing.
Establishes a goal-based framework for MASS design, operation and certification, including modes, operational limits, remote centres, cybersecurity and human oversight.