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  #61 (permalink)  
Old 06-November-2007, 07:34 PM
peter eldergill peter eldergill is offline
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Sorry, I was just trying to be nice to the new guy.
Tee hee...look at your own join date

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  #62 (permalink)  
Old 07-November-2007, 01:50 PM
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According to him, the space shuttle actually visits several space stations each flight. It goes to the secret ones first, because it takes 72 hours for the shuttle to dock at the station, when it should only take them a few hours.
LOL. I've actually docked the ISS and the Shuttle on a few occasions (STS-108, STS-111, STS-113). As we say in the industry, "orbital mechanics is a *****." It takes ~3 days for the Shuttle to get to the ISS. Period. It's no different for Russian Soyuz or Progress vehicles.

Even if there were secret space stations, they'd have to be at an inclination of 51.6 degrees (like the ISS) to support Lear's theory - changing the inclination of a vehicle once in orbit is basically impossible. They'd have to be at different altitudes or the Shuttle couldn't use the same launch window for both. If they're at different altitudes, they'd be traveling at different speeds. If there were any truth to this, you could look up at the night sky and see one appearing to overtake the other.

But you can't. What are the odds that Coast to Coast wants to hear my reasoned explanation?
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  #63 (permalink)  
Old 07-November-2007, 06:36 PM
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LOL. I've actually docked the ISS and the Shuttle on a few occasions (STS-108, STS-111, STS-113). As we say in the industry, "orbital mechanics is a *****." It takes ~3 days for the Shuttle to get to the ISS. Period. It's no different for Russian Soyuz or Progress vehicles.
For real?
That's amazing!
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  #64 (permalink)  
Old 07-November-2007, 08:24 PM
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As we say in the industry, "orbital mechanics is a *****."

I assume that stands for "...harsh mistress."

It takes ~3 days for the Shuttle to get to the ISS. Period. It's no different for Russian Soyuz or Progress vehicles.

Direct ascent to rendezvous is theoretically possible, but only in the sense that it's theoretically possible to throw a ball bearing across the room and hit the light switch so as to turn it off. Because the passive vehicle's orbit is almost never harmonic with the ascending vehicle's position at launch along a rotating Earth, the launch windows would be excessively infrequent and narrow -- prohibitively so for any practical mission.

What are the odds that Coast to Coast wants to hear my reasoned explanation?

Probably about the same as the odds you could throw a ball bearing across the room and turn off the light switch with it.
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  #65 (permalink)  
Old 08-November-2007, 04:37 PM
DrivinWest DrivinWest is offline
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Direct ascent to rendezvous is theoretically possible, but only in the sense that it's theoretically possible to throw a ball bearing across the room and hit the light switch so as to turn it off. Because the passive vehicle's orbit is almost never harmonic with the ascending vehicle's position at launch along a rotating Earth, the launch windows would be excessively infrequent and narrow -- prohibitively so for any practical mission.
Plus you've got to dock, not just knock the passive vehicle out of the sky! While it would be possible to intercept the ISS more quickly, traveling in any direction other than the same exact same velocity vector is the makings for very expensive space debris.

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What are the odds that Coast to Coast wants to hear my reasoned explanation?

Probably about the same as the odds you could throw a ball bearing across the room and turn off the light switch with it.
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  #66 (permalink)  
Old 08-November-2007, 05:11 PM
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Plus you've got to dock, not just knock the passive vehicle out of the sky!

Exactly. Coincident points in space comprise only half the equation. You have first- and possibly second-derivative continuity constraints that translate to velocity and acceleration target values.

Continuing the ball-bearing analogy, if you're across the room throwing a ball bearing, some combination of velocity and arc that is dictated by the goal of getting the ball bearing from where you are all the way across the room to the light switch may not be compatible with the constraint of providing enough force to operate the switch but not too much so that you break the switch. If you have to throw that sucker hard in order to get it several meters away, it's going to break something when it hits.

Thus adds to the harsh mistressitude of orbital mechanics and the reason why ascent and rendezvous are done in phases.
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  #67 (permalink)  
Old 08-November-2007, 05:37 PM
Joe Durnavich Joe Durnavich is offline
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For the planned manned missions to the moon, where they will do 2 launches, will it still take around 3 days for the second vehicle to rendevouz with the first?
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  #68 (permalink)  
Old 08-November-2007, 06:10 PM
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LOL. I've actually docked the ISS and the Shuttle on a few occasions (STS-108, STS-111, STS-113).
As a ground controller or an astronaut? I assume the former, since there were other dockings for the ISS crews between 108 and 113, and since you clearly weren't part of the shuttle only crews for each of those three.
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  #69 (permalink)  
Old 09-November-2007, 08:21 AM
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As a ground controller or an astronaut? I assume the former, since there were other dockings for the ISS crews between 108 and 113, and since you clearly weren't part of the shuttle only crews for each of those three.
Just a ground controller *sigh* - I used to be an ADCO for the ISS.
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  #70 (permalink)  
Old 09-November-2007, 03:15 PM
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For the planned manned missions to the moon, where they will do 2 launches, will it still take around 3 days for the second vehicle to rendevouz with the first?

I searched unsuccessfully for an answer from mission planning. My guess is that they will not take so long.

The ISS orbit is consistent with its overall mission as a long-term habitat for scientific and engineering research. While resupply mission rendezvous is obviously a constraint, it would have to be secondary since there's no way to plan an orbit favorable for all subsequent rendezvouses. Therefore the ascending vehicle has the burden to adapt its orbit, which requires the 3-day nominal harmonization period.

The initial launch of a second-generation Moon mission has one subsequent rendezvous as a primary mission constraint. Therefore its target orbit can be adjusted to make such a rendezvous more favorable for the ascending second launch, along with the additional constraints of orbital stability and compatibility with the planned translunar trajectory. You can plan both launches and orbits together as a single unit mission and adjust both to make the rendezvous as easy as it has to be.
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  #71 (permalink)  
Old 09-November-2007, 07:43 PM
Joe Durnavich Joe Durnavich is offline
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Thanks. I wondered if a 3 day wait would cause a problem with, say, liquid hyrdogen boiling off.
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  #72 (permalink)  
Old 09-November-2007, 10:31 PM
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Just a ground controller *sigh* - I used to be an ADCO for the ISS.
It's okay, I still think your job is wicked cool.
(Yes, I have spent a lot of time in New England)
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  #73 (permalink)  
Old 09-November-2007, 10:51 PM
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Just a ground controller *sigh* - I used to be an ADCO for the ISS.
[
It's okay, I still think your job is wicked cool.
Agreed! (Besides, as anyone in any industry knows, it's the people in the trenches that do the real work --- the famous people just get all the credit)
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  #74 (permalink)  
Old 09-November-2007, 11:24 PM
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Thus adds to the harsh mistressitude of orbital mechanics and the reason why ascent and rendezvous are done in phases.
Novelty alert: Google found one reference to "mistressitude" elsewhere on the web (it hasn't indexed this yet) and it found no references to "harsh mistressitude."
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  #75 (permalink)  
Old 10-November-2007, 12:17 AM
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It's a perfectly cromulent word.
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  #76 (permalink)  
Old 10-November-2007, 12:44 AM
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(snip) and it found no references to "harsh mistressitude."
Maybe you were looking in the wrong places...
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  #77 (permalink)  
Old 10-November-2007, 12:55 AM
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It's a perfectly cromulent word.
"Cromulent" is not in my dictionary.
I guess "harsh mistresstude" is like "That's frierd. It's freaky, and wierd."
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  #78 (permalink)  
Old 10-November-2007, 01:10 AM
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"Cromulent" is not in my dictionary.
I guess "harsh mistresstude" is like "That's frierd. It's freaky, and wierd."
http://dictionary.reference.com/browse/cromulent
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  #79 (permalink)  
Old 10-November-2007, 06:46 AM
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"Cromulent" is not in my dictionary.
I guess "harsh mistresstude" is like "That's frierd. It's freaky, and wierd."
If you can't find it in the dictionary, it's time to google it. In this case, it's also a hint about the joke that you can't find it in the dictionary. It's a Simpson's reference. From the urban dictionary:

Cromulent

Used in an ironical sense to mean legitimate, and therefore, in reality, spurious and not at all legitimate. Assumes common knowledge of the inherent Simpsons reference.
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  #80 (permalink)  
Old 13-November-2007, 11:29 PM
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I love this place! Conspiracy theory debunking and Simpsons references. Awesome!
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Old 13-November-2007, 11:56 PM
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...and don't forget the orbital mechanics tutorials!
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Old 14-November-2007, 01:37 AM
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I love this place! Conspiracy theory debunking and Simpsons references. Awesome!
That's not all! We've got Star Wars quotes and discussions of superheroes powers, too! BAUT is a really fun place!
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