We weren't talking about the Demo model. We were discussing the dimensions of the possible full size model. The Demo model was proposed by Bigelow. I think it would be safe to assume that if the Bigelow Demo design is validated in those tests, Bigelow will build the full size model.
Quote from: Robotbeat on 04/07/2011 02:00 pmQuote from: e of pi on 04/07/2011 01:04 pmI'm not sure how well a Bigelow module would fit on the Falcon Heavy. My best calculations from publicly available data indicate such a 53 ton module would have a usable volume of about 883 cubic meters, which is certainly an interestingly large number. However, to fit within the Falcon's currently announced payload fairing, it might have to have a much higher length:diameter ratio than any of their other modules.Custom fairings are available.Well, in that case, my best guess at a Falcon Heavy-max Bigelow unit would be a 9 m by 18 m module with about 890 cubic meters of volume. It might fit inside of the barrel diameter of the current faring, but would require a stretch of the cylindrical portion to almost triple the current length. A larger diameter fairing could get a larger diameter module, with a shorter length.
Quote from: e of pi on 04/07/2011 01:04 pmI'm not sure how well a Bigelow module would fit on the Falcon Heavy. My best calculations from publicly available data indicate such a 53 ton module would have a usable volume of about 883 cubic meters, which is certainly an interestingly large number. However, to fit within the Falcon's currently announced payload fairing, it might have to have a much higher length:diameter ratio than any of their other modules.Custom fairings are available.
I'm not sure how well a Bigelow module would fit on the Falcon Heavy. My best calculations from publicly available data indicate such a 53 ton module would have a usable volume of about 883 cubic meters, which is certainly an interestingly large number. However, to fit within the Falcon's currently announced payload fairing, it might have to have a much higher length:diameter ratio than any of their other modules.
Dry mass [BA2100] is approximately 65 metric tons...70 metric ton capable launch vehicle will allow initial launch of the vehicle and 10% of water required for supplemental radiation shield.
It would be nice if someone could clear up all the confusion about the various Bigelow proposals, such as what is the relationship of Sundancer to the BA-330 or Nautilus, or any of the other names that have been thrown about as ready to launch Real Soon Now?
Robert Bigelow’s Keynote Address at the 2011 ISDC Governors’ Gala:http://moonandback.com/2011/06/02/robert-bigelows-keynote-address-at-the-2011-isdc-governors-gala/
Quote from: yg1968 on 06/05/2011 08:35 pmRobert Bigelow’s Keynote Address at the 2011 ISDC Governors’ Gala:http://moonandback.com/2011/06/02/robert-bigelows-keynote-address-at-the-2011-isdc-governors-gala/I like this guy.
Dear God, that is awesome. I...words fail me.That's just awesome.
Quote from: Diagoras on 06/06/2011 01:26 amDear God, that is awesome. I...words fail me.That's just awesome.It'll be awesome when and if it happens.
Quote from: Robotbeat on 06/06/2011 01:50 amQuote from: Diagoras on 06/06/2011 01:26 amDear God, that is awesome. I...words fail me.That's just awesome.It'll be awesome when and if it happens.Oh? Do you know something I don't?