GB1439368A - Liquid propellant rocket propulsion unit - Google Patents
Liquid propellant rocket propulsion unitInfo
- Publication number
- GB1439368A GB1439368A GB3257873A GB3257873A GB1439368A GB 1439368 A GB1439368 A GB 1439368A GB 3257873 A GB3257873 A GB 3257873A GB 3257873 A GB3257873 A GB 3257873A GB 1439368 A GB1439368 A GB 1439368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hydrazine
- rocket
- fluorine
- container
- combustion chamber
- 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.)
- Expired
Links
- 239000003380 propellant Substances 0.000 title abstract 7
- 239000007788 liquid Substances 0.000 title abstract 2
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 abstract 16
- 238000000354 decomposition reaction Methods 0.000 abstract 7
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 abstract 5
- 238000002485 combustion reaction Methods 0.000 abstract 5
- 229910052731 fluorine Inorganic materials 0.000 abstract 5
- 239000011737 fluorine Substances 0.000 abstract 5
- 235000015842 Hesperis Nutrition 0.000 abstract 3
- 235000012633 Iberis amara Nutrition 0.000 abstract 3
- 239000007800 oxidant agent Substances 0.000 abstract 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract 1
- 239000003054 catalyst Substances 0.000 abstract 1
- 238000006243 chemical reaction Methods 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 239000001301 oxygen Substances 0.000 abstract 1
- 229910052760 oxygen Inorganic materials 0.000 abstract 1
- UJMWVICAENGCRF-UHFFFAOYSA-N oxygen difluoride Chemical compound FOF UJMWVICAENGCRF-UHFFFAOYSA-N 0.000 abstract 1
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
-
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/68—Decomposition chambers
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19722241424 DE2241424C3 (de) | 1972-08-23 | 1972-08-23 | Verfahren zum Betreiben eines Flüssigkeitsraketentriebwerkes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1439368A true GB1439368A (en) | 1976-06-16 |
Family
ID=5854307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3257873A Expired GB1439368A (en) | 1972-08-23 | 1973-07-09 | Liquid propellant rocket propulsion unit |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2241424C3 (enrdf_load_stackoverflow) |
| FR (1) | FR2197118B1 (enrdf_load_stackoverflow) |
| GB (1) | GB1439368A (enrdf_load_stackoverflow) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2226999A (en) * | 1988-12-16 | 1990-07-18 | Gen Electric | Spacecraft with increased stationkeeping fuel load |
| GB2272488A (en) * | 1992-11-04 | 1994-05-18 | Europ Propulsion | System for feeding reignitable rocket engines |
| US5417049A (en) * | 1990-04-19 | 1995-05-23 | Trw Inc. | Satellite propulsion and power system |
| GB2293627A (en) * | 1990-04-19 | 1996-04-03 | Trw Inc | High performance dual mode rocket propulsion system |
| EP0919464A1 (en) * | 1997-11-25 | 1999-06-02 | TRW Inc. | Spacecraft attitude and velocity control thruster system |
| WO2000058619A1 (en) * | 1999-03-26 | 2000-10-05 | Alliant Techsystems Inc. | Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| EP1172545A1 (de) * | 2000-07-15 | 2002-01-16 | Astrium GmbH | Zündsystem für Brennkammern in Raketentriebwerken |
| EP1283347A1 (fr) * | 2001-08-07 | 2003-02-12 | L'AIR LIQUIDE, Société Anonyme à Directoire et Conseil de Surveillance pour l'Etude et l'Exploitation des | Système propulsif annexe d'étage cryotechnique de lanceur et étage de lanceur comprenant un tel système |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB8609228D0 (en) * | 1986-04-16 | 1986-05-21 | Marconi Co Ltd | Thrusters |
| GB8610849D0 (en) * | 1986-05-02 | 1986-08-20 | Marconi Co Ltd | Gas thruster |
| JPH01500531A (ja) * | 1986-06-19 | 1989-02-23 | ヒユーズ・エアクラフト・カンパニー | 複合形宇宙航行体制御システム |
| DE102005005156B4 (de) * | 2005-02-04 | 2007-06-06 | Astrium Gmbh | Triebwerk |
| CN107701330B (zh) * | 2017-09-14 | 2019-08-09 | 北京控制工程研究所 | 一种不基于气体旁路的系统混合比主动控制方法 |
-
1972
- 1972-08-23 DE DE19722241424 patent/DE2241424C3/de not_active Expired
-
1973
- 1973-07-09 GB GB3257873A patent/GB1439368A/en not_active Expired
- 1973-08-22 FR FR7330512A patent/FR2197118B1/fr not_active Expired
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2226999B (en) * | 1988-12-16 | 1992-05-27 | Gen Electric | Spacecraft with increased stationkeeping fuel load |
| US5263666A (en) * | 1988-12-16 | 1993-11-23 | General Electric Co. | Spacecraft with increased stationkeeping fuel load |
| GB2226999A (en) * | 1988-12-16 | 1990-07-18 | Gen Electric | Spacecraft with increased stationkeeping fuel load |
| US5572865A (en) * | 1990-04-19 | 1996-11-12 | Trw Inc. | Satellite propulsion and power system |
| US5417049A (en) * | 1990-04-19 | 1995-05-23 | Trw Inc. | Satellite propulsion and power system |
| GB2293627A (en) * | 1990-04-19 | 1996-04-03 | Trw Inc | High performance dual mode rocket propulsion system |
| GB2293627B (en) * | 1990-04-19 | 1996-08-21 | Trw Inc | High performance dual mode rocket propulsion system |
| GB2272488B (en) * | 1992-11-04 | 1996-11-20 | Europ Propulsion | An optimized system for feeding a reignitable rocket engine |
| GB2272488A (en) * | 1992-11-04 | 1994-05-18 | Europ Propulsion | System for feeding reignitable rocket engines |
| EP0919464A1 (en) * | 1997-11-25 | 1999-06-02 | TRW Inc. | Spacecraft attitude and velocity control thruster system |
| WO2000058619A1 (en) * | 1999-03-26 | 2000-10-05 | Alliant Techsystems Inc. | Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| US6393830B1 (en) | 1999-03-26 | 2002-05-28 | Alliant Techsystems Inc. | Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines |
| EP1172545A1 (de) * | 2000-07-15 | 2002-01-16 | Astrium GmbH | Zündsystem für Brennkammern in Raketentriebwerken |
| US6564542B2 (en) | 2000-07-15 | 2003-05-20 | Astrium Gmbh | Ignition system for combustion chambers of rocket engines |
| EP1283347A1 (fr) * | 2001-08-07 | 2003-02-12 | L'AIR LIQUIDE, Société Anonyme à Directoire et Conseil de Surveillance pour l'Etude et l'Exploitation des | Système propulsif annexe d'étage cryotechnique de lanceur et étage de lanceur comprenant un tel système |
| FR2828524A1 (fr) * | 2001-08-07 | 2003-02-14 | Air Liquide | Systeme propulsif annexe d'etage cryotechnique de lanceur et etage de lanceur comprenant un tel systeme |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2197118B1 (enrdf_load_stackoverflow) | 1978-01-06 |
| DE2241424B2 (de) | 1977-10-06 |
| DE2241424A1 (de) | 1974-03-07 |
| DE2241424C3 (de) | 1978-06-22 |
| FR2197118A1 (enrdf_load_stackoverflow) | 1974-03-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1439368A (en) | Liquid propellant rocket propulsion unit | |
| US6047541A (en) | HAN TEAN (xm-46) mixing gas generator propellant tank pressurizer for launch vehicles and spacecraft | |
| GB1405847A (en) | Dual thrust level monopropellant spacecraft propulsion system | |
| EP1173668B1 (en) | Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines | |
| US2573471A (en) | Reaction motor operable by liquid propellants and method of operating it | |
| US2408111A (en) | Two-stage rocket system | |
| EP0242196B1 (en) | Thrusters | |
| US5640844A (en) | Pressurization and control devices using high vapor pressure liquids | |
| US2935846A (en) | Reaction motor feed system | |
| US3350887A (en) | Two-stage rocket propulsion system | |
| GB1224633A (en) | Thermodynamic reaction propulsion means | |
| US4787579A (en) | Gas thruster | |
| GB1102625A (en) | Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles | |
| US3695041A (en) | Two-stage hydrazine rocket motor | |
| US2771739A (en) | Rocket propulsion method | |
| GB1210601A (en) | Rocket propulsion system | |
| US3088272A (en) | Stable propellants | |
| US3107485A (en) | Propulsion means and method for space vehicles employing a volatile alkene and metalcarbonyl | |
| GB1320766A (en) | Rocket propulsion system | |
| US10731605B1 (en) | Monopropellant cascade rocket engine | |
| Bloom Jr et al. | Hydrogen peroxide as a propellant | |
| US3170281A (en) | Method of producing thrust by hydrogenation of an acetylenic hydrocarbon | |
| GB2190141A (en) | Spacecraft thruster system | |
| US2896401A (en) | Rocket propulsion method | |
| US2896407A (en) | Rocket propulsion method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |