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SU1740251A1 - Non-expendable aerospace take-off system, flying vehicle of aerospace system - Google Patents

Non-expendable aerospace take-off system, flying vehicle of aerospace system Download PDF

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Publication number
SU1740251A1
SU1740251A1 SU894754826A SU4754826A SU1740251A1 SU 1740251 A1 SU1740251 A1 SU 1740251A1 SU 894754826 A SU894754826 A SU 894754826A SU 4754826 A SU4754826 A SU 4754826A SU 1740251 A1 SU1740251 A1 SU 1740251A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aerospace
aircraft
take
orbit
expendable
Prior art date
Application number
SU894754826A
Other languages
Russian (ru)
Inventor
Виталий Владимирович Андреев
Original Assignee
В.В. Андреев
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 В.В. Андреев filed Critical В.В. Андреев
Priority to SU894754826A priority Critical patent/SU1740251A1/en
Application granted granted Critical
Publication of SU1740251A1 publication Critical patent/SU1740251A1/en

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Abstract

Изобретение относитс  к космической и авиационной технике, в частности к конструкци м космических взлетных систем и кораблей, и может быть использовано дл  доставки на орбиту и с орбиты на Землю грузов. Целью изобретени   вл етс  снижение энергетических затрат при доставке грузов на орбиту и улучшение функционального взаимодействи  и маневренности систем. Система состоит из летательного аппарата 1 с вакуумной энергетической установкой 2, подсоединенного к стартовой направл ющей 3, и соединенных со стартовой направл ющей 3 аэростатических оболочек 4. Летательный аппарат 1 содержит корпус в виде диска с каплевидным поперечным профилем. 2 с.п. ф-лы, 4 ил. gThe invention relates to aerospace and aeronautical engineering, in particular to the structures of spaceborne systems and ships, and can be used to deliver cargoes into orbit and from orbit to Earth. The aim of the invention is to reduce energy costs during the delivery of cargo into orbit and to improve the functional interaction and maneuverability of the systems. The system consists of an aircraft 1 with a vacuum power installation 2 connected to the starting guide 3 and connected to the starting guide 3 of the aerostatic shells 4. The aircraft 1 has a disk-shaped body with a teardrop-shaped transverse profile. 2 sec. f-ly, 4 ill. g

Description

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11eleven

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Claims (2)

Формула изобретенияClaim 1. Воздушно-космическая взлетная система многократного применения, содержащая несколько аэростатических оболочек, связанных между собой стартовой направляющей, расположенной под ними и летательный аппарат, соединенный с направляющей, о тли чающаяся тем, что, с целью снижения энергетических затрат при дос- тавке на орбиту полезных грузов, аэро· статические оболочки выполнены вакуумируемыми и их внутренние полости1. A reusable aerospace take-off system containing several aerostatic shells interconnected by a launch guide located under them and an aircraft connected to the guide, characterized in that, in order to reduce energy costs when delivered to orbit payloads, aero · static shells are evacuated and their internal cavities 5 соединены шлангами с вакуумной энергетической установкой летательного аппарата,5 are connected by hoses to a vacuum power plant of the aircraft, 2. Летательный аппарат воздушнокосмической взлетной системы многоIQ кратного применения, содержащий корпус с каплевидным поперечным профилем, вакуумную Энергетическую установку, двигатели, расположенные внутри корпуса, кили и систему управле15 ния, отличающийся тем, что .он снабжен стартовыми ускорителями, корпус летательного аппарата выполнен в виде диска С крылом, при е этом двигатели, кили и ускорители 20 {расположены на концах крыла.2. Aircraft of the aerospace take-off system of multiple application, containing a body with a drop-shaped transverse profile, a vacuum power plant, engines located inside the body, keels and a control system, characterized in that it is equipped with launch accelerators, the body of the aircraft is made in the form of a disk With a wing, with e engines, keels and accelerators 20 {located at the ends of the wing. А-А фиг. UA-A of FIG. U
SU894754826A 1989-09-27 1989-09-27 Non-expendable aerospace take-off system, flying vehicle of aerospace system SU1740251A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU894754826A SU1740251A1 (en) 1989-09-27 1989-09-27 Non-expendable aerospace take-off system, flying vehicle of aerospace system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU894754826A SU1740251A1 (en) 1989-09-27 1989-09-27 Non-expendable aerospace take-off system, flying vehicle of aerospace system

Publications (1)

Publication Number Publication Date
SU1740251A1 true SU1740251A1 (en) 1992-06-15

Family

ID=21477389

Family Applications (1)

Application Number Title Priority Date Filing Date
SU894754826A SU1740251A1 (en) 1989-09-27 1989-09-27 Non-expendable aerospace take-off system, flying vehicle of aerospace system

Country Status (1)

Country Link
SU (1) SU1740251A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000034122A1 (en) * 1998-12-05 2000-06-15 Fuersich Manfred Method for transporting a payload into outer space
EA009128B1 (en) * 2005-12-12 2007-10-26 Валентин Афанасьевич Сухолитко Methods of take-off and landing of aerial vehicles

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Патент СПА № 1340053, кл. 244-6, 1920. . Патент GB Р 2014529, кл. В 64 В 1/62, 1979. *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000034122A1 (en) * 1998-12-05 2000-06-15 Fuersich Manfred Method for transporting a payload into outer space
EA009128B1 (en) * 2005-12-12 2007-10-26 Валентин Афанасьевич Сухолитко Methods of take-off and landing of aerial vehicles

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