RU2004105332A - METHOD FOR REGULATING THE HYBRID ROCKET ENGINE THrust - Google Patents
METHOD FOR REGULATING THE HYBRID ROCKET ENGINE THrust Download PDFInfo
- Publication number
- RU2004105332A RU2004105332A RU2004105332/06A RU2004105332A RU2004105332A RU 2004105332 A RU2004105332 A RU 2004105332A RU 2004105332/06 A RU2004105332/06 A RU 2004105332/06A RU 2004105332 A RU2004105332 A RU 2004105332A RU 2004105332 A RU2004105332 A RU 2004105332A
- Authority
- RU
- Russia
- Prior art keywords
- regulating
- rocket engine
- engine thrust
- thrust
- hybrid rocket
- Prior art date
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- Engine Equipment That Uses Special Cycles (AREA)
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004105332/06A RU2274761C2 (en) | 2004-02-24 | 2004-02-24 | Method to control ratio of propellant components in hybrid propellant rocket engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004105332/06A RU2274761C2 (en) | 2004-02-24 | 2004-02-24 | Method to control ratio of propellant components in hybrid propellant rocket engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2004105332A true RU2004105332A (en) | 2005-08-10 |
RU2274761C2 RU2274761C2 (en) | 2006-04-20 |
Family
ID=35844474
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2004105332/06A RU2274761C2 (en) | 2004-02-24 | 2004-02-24 | Method to control ratio of propellant components in hybrid propellant rocket engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2274761C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114233523A (en) * | 2021-12-09 | 2022-03-25 | 北京航空航天大学 | Method and system for controlling thrust of solid-liquid hybrid engine |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8056319B2 (en) | 2006-11-10 | 2011-11-15 | Aerojet—General Corporation | Combined cycle missile engine system |
RU2492122C2 (en) * | 2011-06-28 | 2013-09-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Combined method of controlling rocket engine fuel consumption with multiple initiation and combined system of fuel consumption control |
RU2511986C2 (en) * | 2012-07-02 | 2014-04-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" (национальный исследовательский университет) (ФГБОУ ВПО "ЮУрГУ" (НИУ)) | Hybrid rocket engine |
RU2569960C1 (en) * | 2014-12-09 | 2015-12-10 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (НИ ТГУ) | Hybrid rocket engine |
RU2598984C2 (en) * | 2015-01-12 | 2016-10-10 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Вятский государственный университет" | Method of increasing hybrid rocket engine thrust |
-
2004
- 2004-02-24 RU RU2004105332/06A patent/RU2274761C2/en not_active IP Right Cessation
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114233523A (en) * | 2021-12-09 | 2022-03-25 | 北京航空航天大学 | Method and system for controlling thrust of solid-liquid hybrid engine |
CN114233523B (en) * | 2021-12-09 | 2022-12-20 | 北京航空航天大学 | Method and system for controlling thrust of solid-liquid hybrid engine |
Also Published As
Publication number | Publication date |
---|---|
RU2274761C2 (en) | 2006-04-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20070225 |