RU2008127555A - CRYOGENIC REFILLING SYSTEM OF THE SPACE OBJECT - Google Patents
CRYOGENIC REFILLING SYSTEM OF THE SPACE OBJECT Download PDFInfo
- Publication number
- RU2008127555A RU2008127555A RU2008127555/06A RU2008127555A RU2008127555A RU 2008127555 A RU2008127555 A RU 2008127555A RU 2008127555/06 A RU2008127555/06 A RU 2008127555/06A RU 2008127555 A RU2008127555 A RU 2008127555A RU 2008127555 A RU2008127555 A RU 2008127555A
- Authority
- RU
- Russia
- Prior art keywords
- vessel
- cavity
- refueling
- jacket
- unit
- Prior art date
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- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Криогенная заправочная система космического объекта, содержащая коммуникации заправки и слива, дренажные, блок арматурный, блок клапанов, блок откачки и агрегат-заправщик, емкость которого выполнена с тремя полостями - полостью сосуда, полостью рубашки для хладагента и полостью теплоизоляции между рубашкой и оболочкой - и оборудована технологическими коммуникациями, отличающаяся тем, что газовые полости сосуда и рубашки сообщены между собой трубопроводом через регулирующий клапан давления, поддерживающий перепад давления между сосудом и рубашкой не выше расчетного давления сосуда.A cryogenic refueling system for a space object containing refueling and drain communications, drainage, a reinforcement unit, a valve block, a pumping unit and a refueling unit, the capacity of which is made with three cavities - a vessel cavity, a shirt cavity for the refrigerant and a heat insulation cavity between the jacket and the shell - and equipped with technological communications, characterized in that the gas cavities of the vessel and the jacket are interconnected by a pipeline through a pressure control valve that maintains a pressure differential between the vessel m and not jacketed vessel above the design pressure.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008127555/06A RU2386890C2 (en) | 2008-07-07 | 2008-07-07 | Spacecraft cryogenic refueling system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008127555/06A RU2386890C2 (en) | 2008-07-07 | 2008-07-07 | Spacecraft cryogenic refueling system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2008127555A true RU2008127555A (en) | 2010-01-20 |
| RU2386890C2 RU2386890C2 (en) | 2010-04-20 |
Family
ID=42120091
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008127555/06A RU2386890C2 (en) | 2008-07-07 | 2008-07-07 | Spacecraft cryogenic refueling system |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2386890C2 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2455206C1 (en) * | 2010-11-17 | 2012-07-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Method of filling space rocket system oxidiser tanks with liquid oxygen |
| EP3829979A4 (en) | 2018-05-25 | 2022-05-18 | Radian Aerospace, Inc. | Earth to orbit transportation system |
| EP3891376A4 (en) | 2018-07-03 | 2022-10-26 | Radian Aerospace, Inc. | Rocket propulsion systems and associated methods |
| RU2734707C1 (en) * | 2020-02-11 | 2020-10-22 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Method for cooling down system of space object operating in vacuum when simulating normal operating conditions |
-
2008
- 2008-07-07 RU RU2008127555/06A patent/RU2386890C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2386890C2 (en) | 2010-04-20 |
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