[amsat-bb] Re: ARISSat-1 - Dumb Question
Rick Tejera
saguaroastro at cox.net
Thu Feb 10 16:35:37 PST 2011
Sent from my iPod
Rick Tejera
Editor, SACnews
Saguaro Astronomy Club
www.saguaroastro.org
K7TEJ
On Feb 10, 2011, at 17:17, "Bob Bruninga" <bruninga at usna.edu> wrote:
>> a retrograde maneuver will remove ARISSsat from
>> the proximity of ISS very very quickly.
>
> It is interesting that any such one-thrust (arm throw) maneuver will then
> intersect the ISS exactly one orbit later. In theory that is. But the
> difference in drag at that low altitude will usually be enough to have a
> safe miss distance on the next and subsequent orbits.
>
> I think that is why most space maneuvers require two burns. One to start a
> new orbit (but it will still intersect the original orbit on every orbit.
> Then a second burn somewhere else in the orbit to get rid of that
> intersecting point?
>
> Bob, WB4APR
>
>>>>> ... Clint. When ARISSAT is released it will stay in the "Plane" of
> ISS
>>> orbit...they will toss it retrograde meaning in the opposite direction
> of
>>> the velocity vector and with its slightly lower velocity the orbit will
>>> start to decrease...this is done so that very quickly the orbits will
> stop
>>> being "prox ops" reasonably fast.
>>>
>>> If so, then I believe as the orbit altitude is reduced, the apparent
>>> velocity increases.....(??) which will cause ARISsat-1 to 'move ahead'
> of the
>>> ISS over a few hours
>>>
>>> But didn't we say the velocity would be less than the ISS due to the
> method
>>> of deploying it against the velocity vector ?
>>>
>>
>> Interesting puzzler, eh? From what I have read in the past, I think this
> their logic.
>>
>> What they are trying to do is to separate the orbits of the ISS and
> ARISSat as quickly as possible, to avoid the potential for a collision.
> Consider the options:
>>
>> 1. Throw it sideways to the ISS orbit. The result is that twice per
> orbit the two spacecraft's paths will cross, side to side. Bad idea.
>>
>> 2. Throw it ahead of the ISS (faster orbit speed). This will raise the
> orbit, slightly, and also make it a bit elliptical (up and down). The
> higher orbit makes the satellite go behind the ISS, but the elliptical shape
> also means that the orbits will cross every orbit (but out of phase, so they
> won't be at the same place when they do). But, then as the ARISSat orbit
> decays, they will get closer and closer, potentially getting back to the
> same place. Not good, either.
>>
>> 3. Throw it behind the ISS (slower orbit). As you note, this will lower
> the orbit (and make it a bit elliptical), and initially the apogee of the
> orbit will intersect that of the ISS. Being in a lower orbit, ARISSat will
> move ahead of the ISS, and over time, as the ARISSat orbit decays, the two
> will diverge even farther. So, this is the safest.
>>
>> At least, I think that's the logic. If not, pass me some of that tuna...
>>
>> Greg KO6TH
>
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