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Dec
11
accepted What would have been required to boost Mir into a stable orbit?
Dec
11
revised What would have been required to boost Mir into a stable orbit?
Explained orbital specifications
Dec
11
revised What would have been required to boost Mir into a stable orbit?
edited body
Dec
11
comment What would have been required to boost Mir into a stable orbit?
How are questions of rocket payload capacity and capability not physics questions, @DavidZ? Sure, there's a newer more specialized site on the SE network, but that surely doesn't make it off topic for 'physics'. Could you elaborate?
Dec
11
comment What would have been required to boost Mir into a stable orbit?
Could anyone please help to validate this?
Dec
9
revised What would have been required to boost Mir into a stable orbit?
added 336 characters in body
Dec
9
revised What would have been required to boost Mir into a stable orbit?
Added edit section
Dec
9
answered What would have been required to boost Mir into a stable orbit?
Dec
9
revised What would have been required to boost Mir into a stable orbit?
Added to attempts
Dec
9
comment What would have been required to boost Mir into a stable orbit?
On a side note, it's extremely frustrating that there are more calculators and information available online for doing this in Kerbal Space Program then there are for doing it in our solar system or even Earth.
Dec
9
revised What would have been required to boost Mir into a stable orbit?
Added attempts section
Dec
9
comment What would have been required to boost Mir into a stable orbit?
This is a valid physics question, and phys.SE has a lot more users (potentially submitting answers) than spaceexp.SE.
Dec
9
revised What would have been required to boost Mir into a stable orbit?
added 3 characters in body
Dec
9
revised What would have been required to boost Mir into a stable orbit?
added 3 characters in body
Dec
9
asked What would have been required to boost Mir into a stable orbit?
Sep
11
awarded  Notable Question
Jul
2
awarded  Curious
Apr
23
awarded  Notable Question
Apr
22
comment How to calculate the velocity needed for a rocket to get to a L1 point (escape a body without orbiting)?
If launched from earth's equator, that would give 459 m/s of angular velocity. The moon rotates with 1024 m/s of velocity, so yes the rocket would need to 'add' 566 m/s in the rotational direction of the moon to simply 'Fall In'. However, I'm looking for the rest of the component, and I suspect that one would not need all 566 m/s if some fancy maneuvers were added.
Apr
21
revised Rocket propelled by a giant monochromatic laser
Edited to mark incorrectness