RU2436714C2 - Space launch complex - Google Patents
Space launch complex Download PDFInfo
- 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
- Authority
- RU
- Russia
- Prior art keywords
- space launch
- launch complex
- studs
- ropes
- counterweights
- Prior art date
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- Jib Cranes (AREA)
- Tents Or Canopies (AREA)
Abstract
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
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
Claims (1)
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 |
Family
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 |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2436714C2 (en) |
-
2010
- 2010-09-30 RU RU2010140184/11A patent/RU2436714C2/en active
Also Published As
Publication number | Publication date |
---|---|
RU2010140184A (en) | 2011-01-10 |
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