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WO2001066413A1 - Systeme d'aeronef de lancement destine au transport, ravitaillement et lancement en l'air d'une fusee porteuse - Google Patents

Systeme d'aeronef de lancement destine au transport, ravitaillement et lancement en l'air d'une fusee porteuse Download PDF

Info

Publication number
WO2001066413A1
WO2001066413A1 PCT/RU2000/000197 RU0000197W WO0166413A1 WO 2001066413 A1 WO2001066413 A1 WO 2001066413A1 RU 0000197 W RU0000197 W RU 0000197W WO 0166413 A1 WO0166413 A1 WO 0166413A1
Authority
WO
WIPO (PCT)
Prior art keywords
carrier
aircraft
fuselage
fueling
launching
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/RU2000/000197
Other languages
English (en)
Russian (ru)
Inventor
Jury Grigorievich Ishkov
Viktor Vasilievich Mikhailov
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of WO2001066413A1 publication Critical patent/WO2001066413A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G5/00—Ground equipment for vehicles, e.g. starting towers, fuelling arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/08—Arrangement of rocket launchers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B64G1/005—Air launch

Definitions

  • s ⁇ de ⁇ z haschem sam ⁇ le ⁇ - n ⁇ si ⁇ el having ⁇ azmeschennye simme ⁇ ichn ⁇ ⁇ n ⁇ si ⁇ eln ⁇ eg ⁇ l ⁇ - d ⁇ ln ⁇ y ⁇ si ⁇ yag ⁇ vye dviga ⁇ eli, us ⁇ an ⁇ vlennye ⁇ yle on the carrier, g ⁇ iz ⁇ n- ⁇ alnye ⁇ uli 8 form ve ⁇ i ⁇ alny ⁇ ⁇ iley, ⁇ livnye ba ⁇ i, sis ⁇ emu Controls, chassis, and, at the very least, the
  • Fig. 1 a general view of the aviation complex for transporting goods is shown in the air; on ' fig.2 - view in the plan on fig.1 and on fig.3; - view on the plan on fig.1.
  • Aircraft - the host 1 is composed of the United 5 adjoining 5th section of the main 6th section with the main 7th with the backs of the 8th main part of the hometown of the 9th house
  • ⁇ sn ⁇ vn ⁇ e 8 and d ⁇ lni ⁇ eln ⁇ e 10 carrying ⁇ ylya na ⁇ l ⁇ neny ⁇ d ugl ⁇ m ⁇ , ⁇ avnym 7 - 10 °, ⁇ g ⁇ iz ⁇ n ⁇ aln ⁇ y ⁇ l ⁇ s ⁇ s ⁇ i, ⁇ dyaschey che ⁇ ez ⁇ d ⁇ lnuyu ⁇ s ⁇ yuzelyazha 2 ⁇ ichem on ni ⁇ ⁇ dvesheny ⁇ yag ⁇ vye dviga ⁇ eli May 12, ⁇ i e ⁇ m ⁇ yag ⁇ vye dviga ⁇ eli 12 d ⁇ lni ⁇ eln ⁇ g ⁇ 10 nesuscheg ⁇ ⁇ yla offset of sha ⁇ ma ⁇ n ⁇ m On the other hand, there are 12 main 8 main load carriers.
  • Aircraft - Host 1, Location 8 Aircraft - A carrier 1, Base 1
  • the horizontal steering wheels are made in the form of vertical wings 20 and are mounted on an additional 10 carrying arm, which is symmetrical with an integral fuselage 2.
  • the plane - the carrier 1 picks up the required height of the tarmac and keeps the cargo on the run. After the start of the process, there is a charge in the air from the discharges - from the consumables of the vehicle - from the carrier of the consumables; After leaving the plane - carrier 1, the command “for charging” is supplied and the elements of the fastening of the fastening carrier 4 are disconnected with a commercially available cable.
  • ⁇ zhe ⁇ by ⁇ is ⁇ lz ⁇ van for d ⁇ s ⁇ av ⁇ i sna ⁇ yazhenn ⁇ g ⁇ ⁇ a ⁇ e ⁇ n ⁇ si ⁇ elya in sb ⁇ e with ⁇ smiches ⁇ im ⁇ ablem in e ⁇ va ⁇ ialny ⁇ ay ⁇ n za ⁇ us ⁇ a, za ⁇ av ⁇ i eg ⁇ in v ⁇ zdu ⁇ e and za ⁇ us ⁇ e in ve ⁇ ni ⁇ sl ⁇ ya ⁇ a ⁇ m ⁇ s ⁇ e ⁇ y ⁇ b ⁇ e ⁇ eniya and ⁇ a ⁇ zhe for ⁇ ans ⁇ i ⁇ v ⁇ i ⁇ u ⁇ n ⁇ gaba ⁇ i ⁇ ny ⁇ g ⁇ uz ' ⁇ v and is ⁇ lz ⁇ vanie for eg ⁇ s ⁇ zdaniya ⁇ ns ⁇ u ⁇ ivny ⁇ elemen ⁇ v already e ⁇ s ⁇ l ⁇ a ⁇ i ⁇ uemy ⁇ ⁇ yazhely ⁇

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Tires In General (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

L'invention concerne des cargos aériens destinés au transport de fusées porteuses équipées de grandes dimensions dans les zones optimales de lancement ainsi qu'au ravitaillement desdites fusées et de leur lancement dans l'espace à partir des couches supérieures de l'atmosphère. Selon l'invention, le système d'aéronef de lancement destiné au transport, ravitaillement et lancement en l'air d'une fusée porteuse comprend un avion cargo sur lequel est fixée une fusée porteuse contenant le véhicule spatial. L'avion cargo comprend une section avant du fuselage et une aile principale de l'avion 'Antée' et une section arrière du fuselage avec une aile supplémentaire, installée en tandem avec l'aile principale, de l'avion 'Rouslan', les deux sections étant reliées par une section intermédiaire. Des moteurs de propulsion sont accrochés aux ailes, et les moteurs des ailes supplémentaires sont disposés en quinconce par rapport à ceux de l'aile principale. Le fuselage comprend une soute commune, à l'intérieur de laquelle sont disposés les instruments et systèmes nécessaires au ravitaillement, à la préparation et à la commande du lancement de la fusée porteuse. Le châssis de l'avion est fait modulaire; il est constitué de sections escamotables installées sur des supports télescopiques et comprenant une section directionnelle du nez de l'avion et des sections avant, intermédiaire ou arrière, disposées symétriques par rapport à l'axe longitudinal du fuselage.
PCT/RU2000/000197 2000-03-09 2000-05-23 Systeme d'aeronef de lancement destine au transport, ravitaillement et lancement en l'air d'une fusee porteuse Ceased WO2001066413A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2000105569 2000-03-09
RU2000105569A RU2158214C1 (ru) 2000-03-09 2000-03-09 Авиационный пусковой комплекс для транспортировки, заправки и запуска в воздухе ракетоносителя

Publications (1)

Publication Number Publication Date
WO2001066413A1 true WO2001066413A1 (fr) 2001-09-13

Family

ID=20231523

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2000/000197 Ceased WO2001066413A1 (fr) 2000-03-09 2000-05-23 Systeme d'aeronef de lancement destine au transport, ravitaillement et lancement en l'air d'une fusee porteuse

Country Status (2)

Country Link
RU (1) RU2158214C1 (fr)
WO (1) WO2001066413A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109502059A (zh) * 2018-11-15 2019-03-22 上海宇航系统工程研究所 一种运载火箭助推器头锥六自由度对接小车

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2223202C2 (ru) * 2001-12-11 2004-02-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" Способ управления транспортировкой изделий с наддутыми газом тонкостенными емкостями авиационными средствами
FR2839946B1 (fr) * 2002-05-24 2004-12-24 Dassault Aviat Ensemble composite de lancement d'une charge utile dans l'espace
RU2265559C1 (ru) * 2005-09-06 2005-12-10 Даниал Кенжетаевич Ахметов Способ запуска многоступенчатой космической ракеты-носителя с использованием самолета-носителя и многоступенчатая ракета-носитель
RU2317227C1 (ru) * 2006-07-25 2008-02-20 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Авиационный комплекс
RU2331552C1 (ru) * 2006-12-05 2008-08-20 Военная академия Ракетных войск стратегического назначения имени Петра Великого Устройство запуска космических аппаратов с помощью самолетного старта
RU2432303C1 (ru) * 2010-03-09 2011-10-27 Александр Афанасьевич Нарижный Способ вывода в космос космических объектов с помощью многоразовой системы и система для многоразового вывода в космос космических объектов
RU2659609C2 (ru) * 2014-07-10 2018-07-03 Михаил Маркович Ковалевский Космическая транспортная система на базе семейства ракет-носителей легкого, среднего и тяжелого классов с воздушным стартом ракет космического назначения с борта экранолета и способ ее функционирования
RU2729912C1 (ru) * 2018-01-29 2020-08-13 Михаил Маркович Ковалевский Универсальная космическая транспортная система на базе семейства ракет космического назначения лёгкого, среднего и тяжёлого классов с запуском ракет-носителей над акваторией мирового океана

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4557444A (en) * 1984-01-09 1985-12-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerospace vehicle
US4836470A (en) * 1983-09-28 1989-06-06 Criswell David R Aerospace vehicle having multiple propulsion systems on a relatively rotatable flying wing
RU2129508C1 (ru) * 1997-01-05 1999-04-27 Петраков Валерий Михайлович Авиационный пусковой комплекс

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4836470A (en) * 1983-09-28 1989-06-06 Criswell David R Aerospace vehicle having multiple propulsion systems on a relatively rotatable flying wing
US4557444A (en) * 1984-01-09 1985-12-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aerospace vehicle
RU2129508C1 (ru) * 1997-01-05 1999-04-27 Петраков Валерий Михайлович Авиационный пусковой комплекс

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
KACHUR P.I.: "Programma vozdushno -kosnicheskogo somoleta 'Zenger', technicheskaya informatsya, novosti zarubezhnoi nauki i tekhniki", SERYA AVIATSIOMAYA I RAKETNAYA, vol. 15, 1990, pages 14 - 18 *
SHUNEIKO I.I.: "Krylatye kosmicheskie korabli. Itosi naukii techniki", SERYA MASHINOSTROENIE RAKETOSTROENIE 1963-1965, 1966, MOSCOW, pages 39 - 41 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109502059A (zh) * 2018-11-15 2019-03-22 上海宇航系统工程研究所 一种运载火箭助推器头锥六自由度对接小车

Also Published As

Publication number Publication date
RU2158214C1 (ru) 2000-10-27

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