A Russian Soyuz 2-1B has launched a GLONASS-M Global Navigation satellite from the Plesetsk Cosmodrome. Launch occurred from Pad 43/4 at the spaceport, with T-0 reported as 00:21... No related posts.
For about 15 years the astronauts are doing scientific research in the ISS for future space population and traveling.The wide variety of research fields include astrobiology, astronomy, human research including space medicine and life sciences, physical sciences, materials science, space weather,...
well turns out you can have an attitude that is good enough for both solar angle and observations ... considering it did a lot of heliophysics it's actually one and the same anyway
but I think it would be worth also mentioning that the telescope had independent targeting and attitude (3-axis stabilization in this case) capability
that's good for many possible orientations and attitude modes, but also so the guys in the Skylab can goof around and vibrations won't translate to the telescope
The difference between those two rotation periods is, BIG SURPRISE! one rotation a year, so it may be easy to switch between them for different types of observations. But is an Earth facing orientation ruled completely out?
it makes sense since it would have to switch between attitude modes during docking... and that gets a lot cheaper if it's already close to (quasi) inertial
and there would be a lot less of propellant (and thrusters) use
which is also important when you don't have a huge gyro and you're running a microgravity lab
understand. That's why I gave the OP a broad answer so that they have to wade through mountains of technical papers to find their answer, as penance for asking such a question
If you compare the pressurized volume of all the space stations launched to their mass, their mass efficiency seem to decrease over time.
In chronological order:
Salyut: (actually seven stations, but practically identical. Salyut 1 numbers are used)
Pressurized volume: 99 m³
Mass 18,425 k...
First of all, space station's mass is ~ 390,000 kg isslive.com/displays/adcoDisplay1.html, that Wiki quote has always been misleading and includes one Space Shuttle orbiter docked to it
it would be interesting to see if all that mass was worth it in all this time, basically if it amortized itself in all this time
say, if it used fuel cells instead of solar power, it didn't recycle,... would it consume more mass for the total metabolic rate and power consumption than it needs to be more self-sufficient