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John Denker wrote:
Here's the scenario: Spacecraft #1 is launched into a nice, circular,
low-earth orbit. Shortly thereafter, spacecraft #2 is launched into
the _same_ orbit. At this point in the story, spacecraft #2 is
keeping
pace with #1, and is simply 90 km in trail.
The flight plan calls for the two craft to rendezvous. At time t,
spacecraft #2 fires its thruster, thereby giving itself a delta v
of 60 km/h, directed toward spacecraft #1 in the obvious way.
Here's the question: Within a km or so, how far apart are the
spacecraft at time t + 90 minutes?
Vis vobiscum.
Here is my thinking - no calculations.
To first order, the original space craft will make one complete orbit in 90 min.
To first order, the extra 90 km/hr is trivial compared to the orbital speed, so it is a minor perturbation. After 90 min it will also have completed one orbit and will be back where it started in 90 min. Since the second rocket is in a slightly larger orbit, a second order correction implies it will take slightly longer to complete the orbit, so it will be slightly farther away than it had been. (After 45 min = half an orbit, the second rock would be almost straight "above" the first). 360 km (from John M) seems a little more than I would have guessed, by I could believe it.
Tim F