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2 175 934

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IPC

(21) (22)

Application

99122780/28, 1999-10-28

(24)

Start date

1999-10-28

(22)

Actual filing date

1999-10-28

(45)

Published

2001-11-20

(72)

Inventor

Bliznjuk V.I.Aleshin E.A.Benderov V.V.Bondarenko N.N.Klimenko V.I.Rostopchin V.V.Chevardov S.G.

(73)

Holder

Obshchestvo S Ogranichennoj Otvetstvennost'Ju

MULTI-MODE AIRCRAFT-BOOSTER FOR AVIATION ROCKET SPACE COMPLEX Russian patent published in 2001 - IPC

Abstract RU 2175934 C2

FIELD: aeronautical and space engineering; space complexes for injection of space objects into orbits. SUBSTANCE: according to invention, supersonic aircraft of integral configuration at smooth conjugation of fuselage and variable-geometry wing; it is provided with all- moving vertical and horizontal tails and power-plant pods. Proposed booster aircraft is made for carrying launch vehicle (having mass of about 50 tons) under fuselage between power-plant pods. Compartment of fuselage may be used for receiving smaller launch vehicle (having masses lesser than 40 tons). Booster aircraft is provided with equipment for performing functions of aircraft command measuring point Booster aircraft may be used for launching rocket (rockets) at supersonic or subsonic speed followed by shifting to mode set by command and measuring point. Provision is made for wide selection of geographic of launch (inclination of orbits) and in-flight refueling. EFFECT: low cost of injection of payload; enhanced adaptability of space rocket complex. 2 cl, 3 dwg

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RU 2 175 934 C2

Authors

Bliznjuk V.I.

Aleshin E.A.

Benderov V.V.

Bondarenko N.N.

Klimenko V.I.

Rostopchin V.V.

Chevardov S.G.

Dates

2001-11-20—Published

1999-10-28—Filed