D
dreada5
Guest
<i>Let's see: larger launch vehicle, control and propulsion systems for capture of Genesis sample return capsule into Earth orbit and rendezvous with ISS, launch of special equipment and/or facilities to ISS to receive said capsule, ISS crew training and safety, Soyuz or Space Shuttle costs for return to Earth, etc. <br /><br />And all of this for solar wind samples. <br /><br />In my opinion, an extra $200 million for your "fly it to ISS" scenario is not an unreasonable estimate. </i><br /><br />The fact is you don't want believe it can be done cheaply. Well it can. You've exaggerated the costs/procedures.<br /><br />If this mission was designed to capitalise on existing knowledge/hardware then you wouldn't need additional conventional hardware/resources. Progressive delta-vee change via multiple elliptical orbits until it gets into ISS's orbit could have been used OR perhaps even aero-braking - then extra propellant wouldn't be needed and nor a larger launcher. If it was planned this way from the beginning - basic ISS examination facilites would already be in place (they would no doubt come in useful again in future). The robotic arm capture/holds it, an astronaut gets video training from JPL and goes out with tools to retrieve collectors. Alternatively if we don't wanna be creative stow it at the ISS until the next shuttle comes up to fit ISS structural components.<br /><br />Simplified? May be, but my point there are ALWAYS options if we open our eyes.