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Baikal (rocket booster)
The Baikal booster (russ. Байкал) is a proposed reusable flyback booster for the Angara rocket family based on the Angara Universal Rocket Module. It was designed by the Molniya Research and Industrial Corporation (NPO Molniya) for the Khrunichev Space centre, reusing the flyback and control system for the reusable Buran orbiter.
== Description ==
The booster would be equipped with an RD-191 rocket engine burning kerosene and liquid oxygen to provide approximately 200 tons of thrust. In addition, it would be equipped with a folding wing stored parallel to the fuselage of the vehicle during the booster stage of the flight. After separation from the Angara launcher's second stage at an altitude of about 75 kilometers and a speed of , the Baikal's wing would rotate 90 degrees and the booster glides in upside down position reducing speed. Once the booster reaches subsonic speeds a U turn is performed and an air-breathing RD-33 jet engine in its nose section is started to fly back to its launching site and make a powered horizontal landing on a runway. Apart from economic advantages, this procedure
greatly reduces the risk of falling space debris. Reducing this risk was important as the Angara
rockets will be launched from the deep inland Plesetsk Cosmodrome.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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