Quote from: hop on 11/28/2010 07:49 pmThe assumption that RMS berthing is easier or cheaper than docking is dubious. The requirements to station keep in the capture box don't appear much less stringent than those required for docking. That's correct.
The assumption that RMS berthing is easier or cheaper than docking is dubious. The requirements to station keep in the capture box don't appear much less stringent than those required for docking.
Quote from: Jorge on 11/28/2010 08:32 pmQuote from: hop on 11/28/2010 07:49 pmThe assumption that RMS berthing is easier or cheaper than docking is dubious. The requirements to station keep in the capture box don't appear much less stringent than those required for docking. That's correct.Is it safer?
Quote from: Ben the Space Brit on 11/28/2010 07:56 amFWIW, a RMS of some kind on the Bigelow station would be useful mainly to help berth cargo vehicles without needing them to have expensive rendezvous and docking hard and software. The assumption that RMS berthing is easier or cheaper than docking is dubious. The requirements to station keep in the capture box don't appear much less stringent than those required for docking. Another factor is that all berthings to date have required a human controlling the arm, while fully autonomous dockings are well proven.
FWIW, a RMS of some kind on the Bigelow station would be useful mainly to help berth cargo vehicles without needing them to have expensive rendezvous and docking hard and software.
I was wondering. To make big telescopes one of the problems is the fairing diameter of current LV. It forced JWST to use a complicated system to deploy its segmented mirror. Could a Bigelow hangar be built, that has the ECLSS protruding on one side, and a 4m ID port on the side? That way you could get all the mirrors and panels with a bunch of EELV launches, then pressurize, and actually assemble it in space, but on a pressurized vessel. You'd only have to divide in pieces with no more than 4m OD, but you might send longer pieces, like structural beams.When you're done assembling, you'd have to cut the habitat in half to let the telescope free. But may be you could send a replacement. You wouldn't need a new ECLSS nor the wall of the 4m port. It's just an idea, but if designing and building the mirror deployment system cost close to a billion, then this system might be cheaper, specially if you use it for more than one mission. Regrettably you'd need a LEO tug, and an EDS to actually put the telescope in the desired orbit, so If there is a Bigelow station, and a LEO tug is developed, this might be a nice expansion option.
Which would necessitate ultraclean and ultraprecise equipment in the Bigelow station. Simply cutting it open would also contaminate the mirror. Anyway, 4m fairings exist, and some as large as 7.2m for EELV have been considered. Rather use a Bigelow as an L2 workshack if at all in this way (even then I'm not sure it's worth it but is a good publicity stunt).
NASA Managers Discuss Prospect of Bigelow Inflatable on ISS - by Pete Harding:http://www.nasaspaceflight.com/2011/01/nasa-managers-discuss-prospect-bigelow-inflatable-iss/ Specific thread:http://forum.nasaspaceflight.com/index.php?topic=23824.0
Quote from: Chris Bergin on 01/14/2011 11:32 pmNASA Managers Discuss Prospect of Bigelow Inflatable on ISS - by Pete Harding:http://www.nasaspaceflight.com/2011/01/nasa-managers-discuss-prospect-bigelow-inflatable-iss/ Specific thread:http://forum.nasaspaceflight.com/index.php?topic=23824.0Ok, one thing that is bothering me, weren't all the Node 4 CBM's with exception of the AFT CBM going to be converted to LIDS? If so, the Bigelow module could not be berthed to the Hub with a PCBM.