RU2436714C2 - Space launch complex - Google Patents

Space launch complex Download PDF

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Publication number
RU2436714C2
RU2436714C2 RU2010140184/11A RU2010140184A RU2436714C2 RU 2436714 C2 RU2436714 C2 RU 2436714C2 RU 2010140184/11 A RU2010140184/11 A RU 2010140184/11A RU 2010140184 A RU2010140184 A RU 2010140184A RU 2436714 C2 RU2436714 C2 RU 2436714C2
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RU
Russia
Prior art keywords
space launch
launch complex
studs
ropes
counterweights
Prior art date
Application number
RU2010140184/11A
Other languages
Russian (ru)
Other versions
RU2010140184A (en
Inventor
Александр Михайлович Гультяев (RU)
Александр Михайлович Гультяев
Original Assignee
Александр Михайлович Гультяев
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.)
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Publication date
Application filed by Александр Михайлович Гультяев filed Critical Александр Михайлович Гультяев
Priority to RU2010140184/11A priority Critical patent/RU2436714C2/en
Publication of RU2010140184A publication Critical patent/RU2010140184A/en
Application granted granted Critical
Publication of RU2436714C2 publication Critical patent/RU2436714C2/en

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  • Tents Or Canopies (AREA)

Abstract

FIELD: transport.
SUBSTANCE: proposed space launch complex comprises masts and flexible ropes. Space vehicles are suspended to said ropes by means of studs. Rotary rods with counterweights are secured to said studs.
EFFECT: expanded performances.
2 dwg

Description

Изобретение относится к космонавтике и служит для старта летающих аппаратов.The invention relates to astronautics and is used to launch flying vehicles.

Техническим решением является увеличение диапазона космодрома.The technical solution is to increase the range of the spaceport.

Достигается тем, что имеет мачты и гибкие тросы и шпильки на концах летательных аппаратов, к которым прикреплены поворотные стержни с противовесами.This is achieved by having masts and flexible cables and pins at the ends of the aircraft, to which rotary rods with counterweights are attached.

На фиг.1 показан космодром, на фиг.2 - разрез А-А.Figure 1 shows the spaceport, figure 2 is a section aa.

Конструкция включает: мачты 1, которые соединяются тросами 2. На тросах 2 висят летательные аппараты 3, на их концах находятся шпильки 4, на которых прикреплены поворотные стержни 5 с противовесами 6. Летательные аппараты 3 имеют двигатели 7.The design includes: masts 1, which are connected by ropes 2. Aircraft 3 hang on the ropes 2, studs 4 are located at their ends, on which rotary rods 5 with counterweights are attached 6. Aircraft 3 have engines 7.

Устройство работает следующим образом: чтобы взлететь с космодрома, нужно включить двигатели 7, тогда стержни поворотные 5 сложатся, то есть повернутся на 90 градусов под действием противовесов 6.The device works as follows: to take off from the cosmodrome, you need to turn on the engines 7, then the pivoting rods 5 will fold, that is, they will rotate 90 degrees under the action of counterweights 6.

Claims (1)

Космодром, отличающийся тем, что имеет мачты, гибкие тросы и шпильки на концах летательных аппаратов, к которым прикреплены поворотные стержни с противовесами. A spaceport, characterized in that it has masts, flexible cables and pins at the ends of aircraft, to which pivot rods are attached with counterweights.
RU2010140184/11A 2010-09-30 2010-09-30 Space launch complex RU2436714C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010140184/11A RU2436714C2 (en) 2010-09-30 2010-09-30 Space launch complex

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010140184/11A RU2436714C2 (en) 2010-09-30 2010-09-30 Space launch complex

Publications (2)

Publication Number Publication Date
RU2010140184A RU2010140184A (en) 2011-01-10
RU2436714C2 true RU2436714C2 (en) 2011-12-20

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ID=44054338

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010140184/11A RU2436714C2 (en) 2010-09-30 2010-09-30 Space launch complex

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RU (1) RU2436714C2 (en)

Also Published As

Publication number Publication date
RU2010140184A (en) 2011-01-10

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