FR2569234A1 - Propulseur-fusee a plusieurs chambres - Google Patents
Propulseur-fusee a plusieurs chambres Download PDFInfo
- Publication number
- FR2569234A1 FR2569234A1 FR7536436A FR7536436A FR2569234A1 FR 2569234 A1 FR2569234 A1 FR 2569234A1 FR 7536436 A FR7536436 A FR 7536436A FR 7536436 A FR7536436 A FR 7536436A FR 2569234 A1 FR2569234 A1 FR 2569234A1
- Authority
- FR
- France
- Prior art keywords
- rocket booster
- refrigerant
- propellant
- chamber
- charges
- Prior art date
- Legal status (The legal status 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 status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/26—Burning control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
- F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19742456721 DE2456721C2 (de) | 1974-11-30 | 1974-11-30 | Mehrkammer-Raketentriebwerk |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2569234A1 true FR2569234A1 (fr) | 1986-02-21 |
Family
ID=5932175
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7536436A Withdrawn FR2569234A1 (fr) | 1974-11-30 | 1975-11-28 | Propulseur-fusee a plusieurs chambres |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE835727A (de) |
DE (1) | DE2456721C2 (de) |
FR (1) | FR2569234A1 (de) |
GB (1) | GB1605168A (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7003942B2 (en) | 2002-09-12 | 2006-02-28 | Snecma Propulsion Solide | System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5386776A (en) * | 1993-02-24 | 1995-02-07 | Thiokol Corporation | Bore mitigants for solid propellant rocket motors |
US8127534B2 (en) | 2008-02-19 | 2012-03-06 | Raytheon Company | Pellet loaded attitude control rocket motor |
US7685940B1 (en) | 2008-03-21 | 2010-03-30 | Raytheon Company | Rocket motor with pellet and bulk solid propellants |
US20110024165A1 (en) | 2009-07-31 | 2011-02-03 | Raytheon Company | Systems and methods for composite structures with embedded interconnects |
US8826640B2 (en) | 2010-11-12 | 2014-09-09 | Raytheon Company | Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof |
CN106870204A (zh) * | 2017-01-19 | 2017-06-20 | 北京航空航天大学 | 固液火箭发动机燃烧室中间扰流装置 |
CN114263548B (zh) * | 2021-12-22 | 2022-07-12 | 宁波天擎航天科技有限公司 | 一种固液混合发动机及飞行器 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2956401A (en) * | 1959-06-12 | 1960-10-18 | Ernest M Kane | Variable thrust rocket motor |
DE2214802A1 (de) * | 1972-03-25 | 1973-09-27 | Dynamit Nobel Ag | Feststoffraketenmotor |
-
1974
- 1974-11-30 DE DE19742456721 patent/DE2456721C2/de not_active Expired
-
1975
- 1975-11-04 GB GB4583675A patent/GB1605168A/en not_active Expired
- 1975-11-19 BE BE0/162002A patent/BE835727A/fr unknown
- 1975-11-28 FR FR7536436A patent/FR2569234A1/fr not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7003942B2 (en) | 2002-09-12 | 2006-02-28 | Snecma Propulsion Solide | System and method of controlling pressure oscillations of hydrodynamic origin for a solid propellant thruster |
Also Published As
Publication number | Publication date |
---|---|
DE2456721A1 (de) | 1982-11-04 |
GB1605168A (en) | 1982-09-08 |
DE2456721C2 (de) | 1983-07-07 |
BE835727A (fr) | 1983-07-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |