The beginning of the Kliper program can be placed in 1994 when a group of scientists at Energia patented the design in August of that year under the description, "Spacecraft for the reentry in the atmosphere of a planet and method of reentry of a spacecraft in the atmosphere of a planet."
This vehicle was to be biconical with a flat bottom that would be the heat shield for atmospheric reentry. It was to consist of the nose, with a conical shield to protect the front of the spacecraft, the main zone, and the body flaps. The main part of the vehicle would provide lift for the craft during atmospheric reentry, with body flaps allowing the pilot to control the spacecraft at that time. The vehicle was to land horizontally and used the principle of lifting bodies for flight. In other words, it was to have no wings, but the spacecraft body itself would function as a wing.