Welcome, Martin!
Thrash points out one aspect, and I agree with it... Traveller ships have an operational aspect not unlike aircraft, both in terms of costs and realistic limits of operation.
The For simplicty, stick to 5 Registry tons per Displacement Ton (Td); in most editions the Displacement Ton is 14 cubic meters or just about 17.8 cubic yards.
Remember, though, that spacecraft have transient stress loads of up to 3-4 times their G rating in atmosphere, and up to double in some non-atmospheric cases. This means massive structural needs in order to stay intact. Few wet-naval craft experience transient G-loads in excess of 3G; even then, that's high storm wave loading on near-harmonic wavelengths... spine breakers. Past a certain point, one can no longer effectively stress the hulls, since the strength of structural members is a function of cross section, and the mass-loading is a function of volume: the square-cube law. Likewise, radiative heating is affected in unhappy ways by the square cube law.
While naval ships suffer from the square cube law, they have the advantage of not having to hold their weight up on the keel, only to push it on the keel.
Spacecraft, however, are like fore-and-aft pod-thruster naval ships: they can produce thrust loads and need to be able to transfer thrust from both ends, and often the middle.
Further, the intense needs for life support are far more like subs than surface craft, or even aircraft. And, like subs, any pressure hull leak is a catastrophic failure. But, unlike subs, there isn't even the possibility of sending divers out to spearhunt food, nor is there water available. (Of course, in sealed LS, water needs to be managed very carefully. Humans release an awful lot... )
But then we have to add the unique hostilities of space: High radiation levels (much of it easily stopped by hull shells). Microids (micro-asteroidals) which can hit with forces comparable to major artillery.
Summary
Aircraft-like: need for full-load hull. Available thrust levels. Potential for sudden multi-G transient loads. Possibility of liquefaction failures of structural members.
Surface Naval Similarities: Travel times. Crew rates.
Submarine Similarities: Life support needs. Results of integrity failures. Isolation from exterior.
Unique to spacecraft: radiation levels. microid damage.