A
arezn99
Guest
najaB:<br />“There are two major obstacles to the plan you've outlined: first, the US does not have an automated rendezvous system so the Delta/Atlas launched payload would have no way to get 'as close as possible'.” <br />No need in automated rendezvous system at all in this case! There are a number of busters (upper stages) that deliver payload from LEO to GTO. I think it is quite possible to use some of the busters (probably, with some modification) to deliver an ISS component close to ISS. Such buster can keep orientation of the ISS component when a Space Shuttle grabs this component with its arm. Space Shuttles did so with the Hubble telescope several times. <br /><br />“Secondly, the Shuttle-launched ISS payloads were designed specifically to be Shuttle launched. The Shuttle provides a very different launch environment than the EELVs do. Reconfiguring ISS modules to be launched on expendable boosters would cost almost as much and take almost as long as it did to build them in the first place.”<br /><br />The ISS components are quite different. Maybe among them are several components that can be reconfigured for EELVs and it would be done quicker and cheaper. <br /><br />