This is EXACTLY what we should be aiming for as a long term goal. We've already taken the first step with the robo assistants on ISS. Once we have their dexterity sufficiently honed, we need to combine them with the VR capability that the pilots of our UAV's use overseas. The goal should be for an astronaut-technician to enter the control room in a comfortable shirt-sleeve environment, don the VR headpiece and gloves, and suddenly he or she IS the robot, seeing right thru the robots eyes and working right thru the robots hands. Once we can do that then the hanger will never HAVE to be pressurized, although it could be if that's what the job needed.
Quote from: Sparky on 10/30/2010 04:03 pmBut that spine is a hollow tunnel, is it not? A BA-2100 designed as a hangar could have that tunnel as a corridor for moving vehicles (such as landers) along a rail system to be moored in their servicing bays, somewhere inside the module. I wouldn't bet on that. I believe that the spine holds many systems, like power distribution, oxygen and ventilation systems, the head, heating and cooling systems, possibly propellant tanks, and who-knows-what more.
But that spine is a hollow tunnel, is it not? A BA-2100 designed as a hangar could have that tunnel as a corridor for moving vehicles (such as landers) along a rail system to be moored in their servicing bays, somewhere inside the module.
http://www.popularmechanics.com/science/space/news/bigelow-aerospace-ba2100-hotel?click=pm_latestBut as large as the BA-330 is, it's dwarfed by the BA-2100, which is six times as large and has multiple decks. The BA-2100's docking ends are about 25 feet in diameter, and one source told PM that the module's dry mass could be as low as 70 tons. In other words, in its uninflated state, it could be placed into orbit by the heavy-lift launcher that the U.S. Senate recently approved for development. The massive structure could then be inflated and subsequently outfitted with materials carried aboard additional launches. With its radiation and micrometeoroid shielding, the BA-2100 could provide a trip for a large crew to the outer solar system.
BA-2100, BA-3240, etc: I'm curious at what (if any) point it becomes better to partition the modules, air-tight. E.G. for micrometeroid puncture on one end of a jumbo module, the whole module pays for it.
So what I should understand is that contrary to my previous post, the larger the module, the less worthwhile it is to partition? As far as depressurisation goes.
Bigelow interested in getting the Canadian government (the CSA) as a customer:http://www.winnipegfreepress.com/canada/breakingnews/bigelow-aerospace-hopes-canada-will-jump-on-board-commercial-space-station-110206714.html
Quote from: yg1968 on 11/26/2010 01:35 pmBigelow interested in getting the Canadian government (the CSA) as a customer:http://www.winnipegfreepress.com/canada/breakingnews/bigelow-aerospace-hopes-canada-will-jump-on-board-commercial-space-station-110206714.htmlWill it have a Candabigelarm?
Remember that silly "Build a Space Station" feature that Bigelow had on their site for a while? In that one of the things you could attach was a Remote Maneuvering Arm. I doubt they'd include that in a game on their site if they didn't at least have a contingency plan to include one on their complete stations.
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.
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.