Two-stage-to-orbit

A two-stage-to-orbit (TSTO) or two-stage rocket is a <a href="/facts/Launch_vehicle/g1GCGFJB">launch vehicle</a> in which two distinct <a href="/facts/Multistage_rocket/WNrmgztj">stages</a> provide propulsion consecutively in order to achieve orbital velocity. It is intermediate between a <a href="/facts/Three-stage-to-orbit/WNrmgztj">three-stage-to-orbit</a> launcher and a hypothetical <a href="/facts/Single-stage-to-orbit/4qPbu35V">single-stage-to-orbit</a> (SSTO) launcher.
At liftoff the first stage is responsible for accelerating the vehicle. At some point the second stage detaches from the first stage and continues to orbit under its own power.
An advantage of such a system over single-stage-to-orbit is that most of the dry mass of the vehicle is not carried into orbit. This reduces the cost involved in reaching orbital velocity, as much of the structure and engine mass is ejected, and a larger percentage of the orbited mass is payload mass.
An advantage over three or more stages is a reduction in complexity and fewer <a href="/facts/Separation_event/WNrmgztj">separation events</a>, which reduces cost and risk of failure.

Two-stage-to-orbit open-in-new

Two-stage-to-orbit