Orbital mechanics
Delta-v, docking geometry, reboost profile, decay timeline, propellant, controllability and safe failure modes.
Review gates
The useful question is: what evidence would make ISS preservation technically, legally, financially and diplomatically credible?
Gates
Delta-v, docking geometry, reboost profile, decay timeline, propellant, controllability and safe failure modes.
Fatigue, pressure integrity, thermal cycling, docking loads, module isolation and what can safely remain operational.
No alternative matters if it increases risk to crew, ground populations, other spacecraft or future LEO operations.
The station is a partner asset. Any path needs partner-agency consent, treaty compliance and diplomatic legitimacy.
Ownership, responsibility, registration, liability, salvage, debris, insurance and end-state governance have to be clear.
The comparison is not a slogan. It needs lifecycle cost, schedule, launch procurement, operations and de-risking estimates.
A preservation case must show why the ISS remains valuable as science infrastructure, orbital museum, training platform or staging node.
AUKUS participation would need a visibly peaceful, civilian-science and partner-led frame, not a militarised orbital claim.
Outputs
A credible preservation concept exists and deserves a formal partner-agency, legal and engineering study.
Some useful lessons or partial preservation options exist, but full ISS preservation is not yet credible.
The answer is no, and the public record explains why the controlled-deorbit baseline remains the responsible choice.