When eventually launched, both boosters and the first stage are designed to return to earth, landing upright for reuse.
That this seems entirely feasible is a testament to how far SpaceX has moved the industry forward (and signifies that they are going to have a huge lead over any competitors).
It's not exactly a new idea. The boosters on the Russian Shuttle equivalent were designed to glide back for reusability in the 70s and 80s, but it's amazing the lack of momentum pushing these ideas forward languished in the space tech arena until SpaceX showed up.
There are many difference between a glide-back booster like the Baikal, and a Falcon 9 first stage.
Baikal would not only need wings and other aerodynamic surfaces, but also was supposed to contain a jet engine. However, perhaps more importantly, it would need to have structural rigidity to bending to be able to fly back horizontally. The result would be a significant mass penalty.
Falcon 9 only needs some landing legs, a little extra heat shielding around the engines, some grid fins, and some extra fuel. As it comes back in tail first, it only needs to be strong in the same direction it needed to be strong when launching. And they can use exactly the same rocket (minus legs and grid fins) in expendible mode where they burn all the fuel to reach orbit rather than saving some for the reentry and landing burns, for payloads that are too heavy to recover the booster.
One thing SpaceX discovered when they first started working on reusability was that high-altitude reentry itself was hard, not just the landing. After booster burnout at about 70km altitude, the first stage is travelling upwards fast enough that it reaches 125km. Their first attempts broke up on reentry, before the parachutes they planned to use were any use. Only by doing a reentry burn could they slow enough to survive to even consider how to land.
If I understood correctly, after booster separation the russian proposal was to fly in an upside down arc starting at 75km using the wing to burn off upwards velocity, so they're not reentering from nearly so high. Would be interesting to see that work - I'm sure they must have done the calculations, but still seems like it must be a pretty hairy reentry.
According to the Russian Wiki article, Energiya's first stage was designed to be reusable by the way of parachutes, solid fuel engines and supports, however, the system was not implemented during its two launches and the parachute containers were loaded with other equipment. Wiki gives this as reference:
http://www.buran.ru/htm/09-3.htm
That this seems entirely feasible is a testament to how far SpaceX has moved the industry forward (and signifies that they are going to have a huge lead over any competitors).