RU2002103848A - REUSABLE AIRCRAFT DRIVER - Google Patents

REUSABLE AIRCRAFT DRIVER

Info

Publication number
RU2002103848A
RU2002103848A RU2002103848/28A RU2002103848A RU2002103848A RU 2002103848 A RU2002103848 A RU 2002103848A RU 2002103848/28 A RU2002103848/28 A RU 2002103848/28A RU 2002103848 A RU2002103848 A RU 2002103848A RU 2002103848 A RU2002103848 A RU 2002103848A
Authority
RU
Russia
Prior art keywords
wings
front wing
engine compartments
compartments
center
Prior art date
Application number
RU2002103848/28A
Other languages
Russian (ru)
Other versions
RU2211784C2 (en
Inventor
Владимир Григорьевич Власенко
Original Assignee
Владимир Григорьевич Власенко
Filing date
Publication date
Application filed by Владимир Григорьевич Власенко filed Critical Владимир Григорьевич Власенко
Priority to RU2002103848/28A priority Critical patent/RU2211784C2/en
Priority claimed from RU2002103848/28A external-priority patent/RU2211784C2/en
Publication of RU2002103848A publication Critical patent/RU2002103848A/en
Application granted granted Critical
Publication of RU2211784C2 publication Critical patent/RU2211784C2/en

Links

Claims (2)

1. Многоразовый летательный аппарат - разгонщик, содержащий несущие плоскости сверхзвуковой аэродинамической формы, с воздушно-реактивными двигателями в качестве маршевой двигательной установки, а также элементами крепления разгоняемого полезного груза, отличающийся тем, что представляет собой "биплан", крылья которого разнесены по продольной и поперечной осям, при этом переднее крыло имеет прямую стреловидность и смещено вверх по оси Y относительно центра масс, а заднее, крыло имеет обратную стреловидность и расположено ниже центра масс, двигательные отсеки, ориентированные по продольной оси изделия, размещены на концах крыльев, соединены между собой крыльями и образуют вместе с ними единую, жесткую конструкцию, причем двигатели оснащены, поворотными соплами-насадками, которые обеспечивают управление вектором тяги, шасси, размещенные в задней по полету части двигательных отсеков, ориентированы для вертикального взлета и посадки, а элементы крепления полезной нагрузки размещены с возможностью ее крепления и отделения во время полета с нижней стороны переднего крыла, при этом источники электропитания, топливные отсеки и навигационное оборудование размещены как в двигательных отсеках, так и в крыльях разгонной ступени.1. A reusable aircraft is an accelerator containing bearing planes of a supersonic aerodynamic shape, with jet engines as a propulsion system, as well as fastening elements of the accelerated payload, characterized in that it is a “biplane”, the wings of which are spaced apart in longitudinal and transverse axes, while the front wing has a direct sweep and is shifted upward along the Y axis relative to the center of mass, and the rear wing has a reverse sweep and is located below the center of the ma c, engine compartments oriented along the longitudinal axis of the product are placed at the ends of the wings, connected by wings and form a single, rigid structure with them, and the engines are equipped with rotary nozzles-nozzles that provide control of the thrust vector, the chassis located in the rear on flight, parts of the engine compartments are oriented for vertical take-off and landing, and the payload fastening elements are placed with the possibility of its fastening and separation during flight from the lower side of the front wing, at the same time, power sources, fuel compartments and navigation equipment are located both in the engine compartments and in the wings of the upper stage. 2. Летательный аппарат-разгонщик по п. 1, отличающийся тем, что на переднем крыле установлены кабины экипажа. 2. Aircraft booster according to claim 1, characterized in that on the front wing there are crew cabs.
RU2002103848/28A 2002-02-18 2002-02-18 Recoverable boost vehicle RU2211784C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2002103848/28A RU2211784C2 (en) 2002-02-18 2002-02-18 Recoverable boost vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2002103848/28A RU2211784C2 (en) 2002-02-18 2002-02-18 Recoverable boost vehicle

Publications (2)

Publication Number Publication Date
RU2002103848A true RU2002103848A (en) 2002-06-20
RU2211784C2 RU2211784C2 (en) 2003-09-10

Family

ID=29777431

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002103848/28A RU2211784C2 (en) 2002-02-18 2002-02-18 Recoverable boost vehicle

Country Status (1)

Country Link
RU (1) RU2211784C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2954275B1 (en) * 2009-12-22 2012-01-13 Astrium Sas ULTRA-RAPID AIR VEHICLE AND ASSOCIATED AIR LOCOMOTION METHOD
RU2544446C1 (en) * 2014-01-22 2015-03-20 Виктор Андреевич Павлов Rolling cruise missile
RU2544447C1 (en) * 2014-01-22 2015-03-20 Виктор Андреевич Павлов Flight method of rolling missile
RU2769791C1 (en) * 2021-05-31 2022-04-06 Дмитрий Сергеевич Дуров Multi-element composite aerospace complex for vertical take-off and landing in the sea launch system

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