![]() |
|
|
Thread Tools | Display Modes |
#20
|
|||
|
|||
![]()
Derek Lyons wrote:
"Jeff Findley" wrote: 5 tons may be a bit tight to develop a pressurized people carrier for a dozen people, but I'd think 6 to 8 people ought to be doable. So what do you think Derek? Sound reasonable to you? 5 tons as a weight seems like a reasonable starting point - but the sticky part is (as I point out to George), 5 tons of what? (I.E. when you get beyond Power Point, volume matters.) A cargo bay 1 meter by 2 is a different matter than one that is 2 meters by 10, even if both are limited to five tons gross capacity. This matters in the 5 tons and orbital assembly scenario greatly. There are some reasonable bounds we can put on the problem, at least. Minimum acceptable volume would start somewhere around the density of water. I don't know of any spacecraft parts or propellants significantly denser than that (peroxide and nitrogen tetroxide and nitric acid are, but not by a large factor). So at least that much volume. Maximum credible volume would be something like the density of a tank full of liquid hydrogen, which is roughly 13.5 cubic meters per ton (assume 12 cu m/ton including a tank). Real tanks are going to have endcaps and the like, but let's for now simplify to those numbers. See, easy, we already almost got it to within an order of magnitude range, in two easy paragraphs ;-) 5 tons at 12 cu m/ton would be 60 cu m. In rough terms, 3 m diameter by 9 or 10 m cargo bay, or 4 m diameter by 5 m long. 5 tons at 1 cu m/ton is 5 cubic meters, which is only going to be something like 1.5 m diameter by 3 m long. If you're putting people in, a seated person plus access space is no less than 1 cu m, more like 2 cu m. You could credibly put at least 1 person per 500 kilograms, perhaps as good as 1 person per 250 kilograms. 5 tons therefore is 10 to 20 people. 10 people at 1 cubic meter per is 10 cubic meters; 20 people at 2 cubic meter per is 40 cubic meters. I think that range is a more reasonable lower bound range. Reasonable realistic minimum is probably somewhere around 20 cubic meters, or say a 2 m diameter 6 m long volume. 2 m is also likely the minimum credible diameter to get berthing module / hatch assemblies which are big enough for people and racks to get through. Where you go from here depends a lot on the RLV design issues. Keep in mind that the Fluffy Capsule arguments work as well on most RLV designs: low density is good, and larger cargo volume may not be a weight or design problem as much as you might think on first analysis of the problem. -george william herbert |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Space Calendar - April 28, 2005 | [email protected] | History | 0 | April 28th 05 05:21 PM |
shuttle C dreming | steve rappolee | Policy | 47 | March 10th 04 12:10 AM |
Clueless pundits (was High-flight rate Medium vs. New Heavy lift launchers) | Rand Simberg | Space Science Misc | 18 | February 14th 04 03:28 AM |
Moon key to space future? | James White | Policy | 90 | January 6th 04 04:29 PM |
Unofficial Space Shuttle Manifest | Steven S. Pietrobon | Space Shuttle | 0 | October 6th 03 02:59 AM |