RU2015117118A - Spacecraft propulsion jet propulsion system - Google Patents
Spacecraft propulsion jet propulsion system Download PDFInfo
- Publication number
- RU2015117118A RU2015117118A RU2015117118A RU2015117118A RU2015117118A RU 2015117118 A RU2015117118 A RU 2015117118A RU 2015117118 A RU2015117118 A RU 2015117118A RU 2015117118 A RU2015117118 A RU 2015117118A RU 2015117118 A RU2015117118 A RU 2015117118A
- Authority
- RU
- Russia
- Prior art keywords
- electrolyzer
- hydrogen
- spacecraft
- current source
- compressor
- Prior art date
Links
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract 14
- 239000001257 hydrogen Substances 0.000 claims abstract 14
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract 14
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract 6
- 239000007788 liquid Substances 0.000 claims abstract 4
- 229920000642 polymer Polymers 0.000 claims abstract 4
- 239000007787 solid Substances 0.000 claims abstract 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000003638 chemical reducing agent Substances 0.000 claims abstract 2
- 239000007789 gas Substances 0.000 claims abstract 2
- 239000001301 oxygen Substances 0.000 claims abstract 2
- 229910052760 oxygen Inorganic materials 0.000 claims abstract 2
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K99/00—Subject matter not provided for in other groups of this subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/401—Liquid propellant rocket engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electrolytic Production Of Non-Metals, Compounds, Apparatuses Therefor (AREA)
Abstract
1. Импульсная реактивная двигательная установка космического аппарата, включающая твердополимерный электролизер воды, вход водородной полости которого гидравлически связан с герметичным резервуаром с водой, имеющим штуцер наддува, газожидкостной сепаратор, подключенный к выходу водородной полости электролизера и связанный с ее входом байпасной гидромагистралью, на которой установлен насос, баллон для хранения водорода и реактивный двигатель, соединенные пневмомагистралью с клапаном, а также управляемый источник тока, подключенный к электролизеру, отличающаяся тем, что в нее введен подключенный к управляемому источнику тока электрохимический компрессор водорода, вход которого пневматически соединен с газовой полостью газожидкостного сепаратора, а выход - с баллоном для хранения водорода и штуцером наддува резервуара с водой пневмомагистралями с клапанами, причем на второй из них установлен также редуктор давления, при этом электрохимический компрессор водорода имеет байпасную разгрузочную пневмомагистраль с клапаном, соединяющую выход компрессора с его входом.2. Импульсная реактивная двигательная установка космического аппарата по п. 1, отличающаяся тем, что выход электролизера по кислороду сообщается с системой жизнеобеспечения космического аппарата, а твердополимерный электролизер и электрохимический компрессор водорода включены последовательно в общую цепь электропитания управляемого источника тока.1. A pulsed rocket propulsion system of a spacecraft, including a solid polymer water electrolyzer, the inlet of the hydrogen cavity of which is hydraulically connected to a sealed water tank having a boost nozzle, a gas-liquid separator connected to the outlet of the hydrogen cavity of the electrolyzer and connected to its input by a bypass hydraulic line on which it is installed a pump, a hydrogen storage cylinder and a jet engine connected by a pneumatic line to the valve, as well as a controlled current source connected electrolyzer, characterized in that an electrochemical hydrogen compressor connected to a controlled current source is introduced into it, the inlet of which is pneumatically connected to the gas cavity of the gas-liquid separator, and the outlet is connected to a hydrogen storage cylinder and a water tank pressurization fitting with pneumatic lines with valves, the second of which they are also equipped with a pressure reducer, while the electrochemical hydrogen compressor has a bypass discharge pneumatic line with a valve connecting the compressor output to its input .2. The pulsed rocket propulsion system of a spacecraft according to claim 1, characterized in that the oxygen output of the electrolyzer communicates with the life support system of the spacecraft, and the solid polymer electrolyzer and an electrochemical hydrogen compressor are connected in series to the power supply circuit of the controlled current source.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2015117118/06A RU2605163C2 (en) | 2015-05-05 | 2015-05-05 | Pulse jet propulsion plant of spacecraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2015117118/06A RU2605163C2 (en) | 2015-05-05 | 2015-05-05 | Pulse jet propulsion plant of spacecraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2015117118A true RU2015117118A (en) | 2016-11-27 |
| RU2605163C2 RU2605163C2 (en) | 2016-12-20 |
Family
ID=57759000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2015117118/06A RU2605163C2 (en) | 2015-05-05 | 2015-05-05 | Pulse jet propulsion plant of spacecraft |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2605163C2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108416125A (en) * | 2018-02-13 | 2018-08-17 | 北京空间技术研制试验中心 | The design and verification method of low rail long-life manned spacecraft |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2673640C1 (en) * | 2017-08-16 | 2018-11-28 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Electrolysis rocket engine unit and method of its operation |
| RU2673920C1 (en) * | 2017-10-05 | 2018-12-03 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Method for creating a reactive thrust of a manned spacecraft |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5279484A (en) * | 1992-03-11 | 1994-01-18 | Loral Aerospace Corporation | Manned space vehicle with low-level hydrogen-oxygen-carbon dioxide propulsion unit |
| RU2215891C2 (en) * | 2001-02-13 | 2003-11-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" | Impulse solar rocket engine installation |
| RU2310768C2 (en) * | 2005-10-07 | 2007-11-20 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" | Impulse-action rocket solar oxygen-hydrogen propulsion plant |
| US20110017874A1 (en) * | 2007-11-26 | 2011-01-27 | Clearvalue Technologies, Inc. | Means of fuel and oxidizer storage |
-
2015
- 2015-05-05 RU RU2015117118/06A patent/RU2605163C2/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108416125A (en) * | 2018-02-13 | 2018-08-17 | 北京空间技术研制试验中心 | The design and verification method of low rail long-life manned spacecraft |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2605163C2 (en) | 2016-12-20 |
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