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(19)

(11)

2 309 088

(13)

(51)

IPC

B64G1/14(2006-01-01)

B64G1/16(2006-01-01)

(21) (22)

Application

2005129230/11, 2005-09-19

(24)

Start date

2005-09-19

(22)

Actual filing date

2005-09-19

(45)

Published

2007-10-27

(72)

Inventor

Vavilin Aleksandr Vasil'EvichUsolkin Jurij Jur'EvichFetisov Vjacheslav Aleksandrovich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Raketnyj Tsentr Im. Akademika V.P. Makeeva"

NON-EXPENDABLE SINGLE-STAGE VERTICAL TAKEOFF AND LANDING LAUNCH VEHICLE Russian patent published in 2007 - IPC B64G1/14 B64G1/16

Abstract RU 2309088 C2

FIELD: non-expendable space systems.

SUBSTANCE: proposed launch vehicle has axisymmetrical body with payload, cruise engine plant and takeoff-and-landing shock absorbers. Mounted between struts of shock absorbers and cruise engine nozzle is heat shield made in form of hollow thin-walled compartment made from heat-resistant material.

EFFECT: minimization of gas dynamic and thermal loads on shock absorbers from working engine during launching and landing; enhanced reliability of shock absorbers at repeated use of launch vehicle (up to 50 times).

1 dwg

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RU 2 309 088 C2

Authors

Vavilin Aleksandr Vasil'Evich

Usolkin Jurij Jur'Evich

Fetisov Vjacheslav Aleksandrovich

Dates

2007-10-27—Published

2005-09-19—Filed