I think we got into this discussion talking about rotating ships, to provide midi-gravity. We know that microgravity requires a lot of effort to counteract, so ... you're going to need some major engineering reasons to not go down the spin-for-pseudo-gravity route.
Yes, centrifugal gravity seems like the only way to stay healthy in space. I pointed out that long-term colonies shouldn't rotate faster than 1 rpm in order to avoid inducing motion sickness. That imposes such serious tensile strength requirements that it seems like the shield can't spin with the ship unless the ship is made of carbon nanotubes.
Take a close look at the design of the ISS (because I've seen those designs online ; other spacecraft will have the same issues) : the radiators protrude in one direction radial to the Sun, but the solar panels are perpendicular to the Sun. If you rotate the system by 90 degrees, then the solar panels are useless and the radiators become heat absorbers. That's probably a large part of the reason for not rotating the ISS, but ... comments above about the effort needed to avoid the health problems of microgravity.
Yes, the ISS is a useful example. I'm proposing a modular design, where a sphere with interior radius of 10.7 meters has enough living and garden space to support 4 people. One sphere alone couldn't provide centrifugal gravity, but in that configuration the solar panels would be unfolded perpendicular to the Sun, and the radiators would be unfolded behind the sphere, radially away from the Sun.
But two spheres could dock and attach tethers at the top of each sphere. Then if they separate to a distance of 1800 meters, they could rotate at 1 rpm around their shared center of mass to produce 1g of centrifugal gravity.
If they're not going anywhere, their plane of rotation should probably be the ecliptic plane. Otherwise the Sun's orientation would change as they orbit the Sun. Each sphere's radiators could be attached to the tethers, parallel to the ecliptic plane so they never face the Sun.
During the docking procedure, each sphere's solar panel would be detached and remain at the midpoint between the spheres. They'd have to be able to move along the tether in case one of the spheres becomes heavier and moves the center of mass. The solar panels would be kept perpendicular to the Sun as the spheres rotate, so they'd have to be kept in place magnetically and transfer power to the spheres using induction or microwaves.
I still don't like relying on rotary joints, particularly coaxial ones. I'd use them where unavoidable, but I'd avoid them where possible. And in life-support, they'd scare me.
Yeah, me too. That's why I spent more time than I'd care to admit trying to think of a way to arrange the solar panels that doesn't require a special magnetic rotary joint. At first I thought the sphere's plane of rotation should have a surface normal that points directly at the Sun. That way the solar panels could be attached directly to the tethers on the side that always faces the Sun, and the radiators could also be attached directly to the tethers, but at 90 degrees so they never face the Sun. They could also be attached to the side of the sphere which never faces the Sun.
That might be an emergency configuration if the magnetic rotary joint fails, but the sphere's plane of rotation stays fixed as they orbit the Sun. That means that in 4 months the configuration will have shifted by 90 degrees, making the solar panels useless.
It would be too expensive to continually use fuel to keep the sphere's plane of rotation in place relative to the Sun. Maybe an electrodynamic tether could work, but I haven't looked at that possibility in detail.
And on your general voyage (no, you don't design a vessel for only one voyage - craft design versus industrial production?) you are going to have a component of travel which is not radial to the Sun. Therefore, essentially all parts of the ship's surface are going to have alternating exposure to light and dark.
I've been considering Hohmann transfer orbits because they only require thrust that's completely tangential to the Sun. In that case, the spheres' plane of rotation would be perpendicular to the ecliptic plane. This way, engines on the "side" of each sphere could provide thrust for the Hohmann transfer. If that thrust is large enough to perceptibly affect the direction of "down" then the spheres could simply tilt to keep the total effective gravity vector "vertical" relative to the sphere's floors. To keep that total effective gravity at exactly 1g, the spheres' rotation rate would have to be slowed.
One huge problem is that the shielding mass required to cover the sphere with 4.5 tons/m^2 is greater than 20,000 metric tons. Even if each sphere had a Saturn V rocket underneath it, it would only accelerate at 0.15 g for a few minutes. A fission or fusion rocket would probably be necessary to achieve any useful delta-v.