tag:blogger.com,1999:blog-8809438035746342262.post7940023942951194795..comments2023-10-27T19:34:05.946-07:00Comments on NEW PAPYRUS: Practical Timelines and Funding for Establishing Permanent Outpost on the Moon and Mars using Propellant Producing Water Depots and SLS and Commercial Launch Capability (Part I)Marcel F. Williamshttp://www.blogger.com/profile/16245086958213100840noreply@blogger.comBlogger2125tag:blogger.com,1999:blog-8809438035746342262.post-89421675418404219612017-10-23T09:30:33.724-07:002017-10-23T09:30:33.724-07:00Thanks for your input Nathan!
I agree, that the ...Thanks for your input Nathan!<br /><br /> I agree, that the 70 tonne capability for the Block 1 is likely to be its minimum payload capability. So a 90 tonnes plus capability for the SLS Block I would not surprise me. <br /><br />Marcel Marcel F. Williamshttps://www.blogger.com/profile/16245086958213100840noreply@blogger.comtag:blogger.com,1999:blog-8809438035746342262.post-55564572047907670792017-10-20T16:26:50.853-07:002017-10-20T16:26:50.853-07:00Just a quick interesting bit- the 70t quoted numbe...Just a quick interesting bit- the 70t quoted number for block 1 subtracts the ICPS. The throw capability of the core+boosters is closer to ~95 tons to LEO! http://www.spacelaunchreport.com/sls0.htmlAnonymoushttps://www.blogger.com/profile/10597033541123354648noreply@blogger.com