[CarolineW]

From Wikipedia:

    The project's long-term objectives include
    returning a launch vehicle first stage to
    the launch site in minutes and to return a
    second stage to the launch pad following
    orbital realignment with the launch site
    and atmospheric reentry in up to 24 hours.

https://en.wikipedia.org/wiki/SpaceX_reusable_launch_system_...

However, from other sources:

    SpaceX would love to recover the second
    stage, which they had planned.  But it
    sounds like they have given up on that.

http://space.stackexchange.com/questions/7814/what-happens-t...

What they are referring to there is a transcript I have been unable to access. It's here:

http://shitelonsays.com/transcript/elon-musk-at-mits-aeroast...

More discussion about it all here:

https://www.quora.com/Could-SpaceX-feasibly-recover-the-seco...

https://www.reddit.com/r/spacex/comments/1zg7zm/how_soon_can...

https://www.google.co.uk/search?q=space-X+recovering+second+...

[jbooth]

Seems way harder for way lower returns to recover the second stage. Only 1 engine instead of 9, and you're recovering from orbital velocity which opens up several new cans of worms. Would they need heat shielding? The extra weight there might blow away any cost savings from recovering the engine.

[jadyoyster]

Heat shielding is needed, as well as extra landing engines that work outside of vacuum, since the second stage engine would destroy itself under atmospheric pressure. It's easy to see how quickly you start to get dimishing returns, but it would be cool if they could pull it off.

[avmich]

Some experiments were done in early 2000 with inflatable aerobrake. The concept was shown to work, but experiments weren't a complete success. However this technology I'm sure can be applied to the task of returning the second stage.

https://en.wikipedia.org/wiki/Atmospheric_entry#Inflatable_h...

[raducu]

Or even more futuristic, plasma parachute/heat shield: http://www.nasa.gov/offices/oct/early_stage_innovation/niac/...