WO2014149184A3 - Procédés et systèmes améliorés de moteurs de fusée à combustion - Google Patents

Procédés et systèmes améliorés de moteurs de fusée à combustion Download PDF

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Publication number
WO2014149184A3
WO2014149184A3 PCT/US2014/013247 US2014013247W WO2014149184A3 WO 2014149184 A3 WO2014149184 A3 WO 2014149184A3 US 2014013247 W US2014013247 W US 2014013247W WO 2014149184 A3 WO2014149184 A3 WO 2014149184A3
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WO
WIPO (PCT)
Prior art keywords
propellant
rocket engine
primary
methods
enhanced combustion
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.)
Ceased
Application number
PCT/US2014/013247
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English (en)
Other versions
WO2014149184A2 (fr
Inventor
Andrew Stephen HOWELLS
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of WO2014149184A2 publication Critical patent/WO2014149184A2/fr
Publication of WO2014149184A3 publication Critical patent/WO2014149184A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Testing Of Engines (AREA)

Abstract

L'invention concerne un système (100) amélioré de moteur de fusée à combustion, qui comprend au moins un réservoir (110) de propergol principal, conçu pour loger un propergol (111) principal, dans un état solide et/ou un état de fusion de transition et/ou un état fondu et pour fournir le propergol (111) principal dans l'état fondu, au moins un réservoir de propergol secondaire, conçu pour loger un propergol secondaire dans un état liquide; et au moins un moteur (140) de fusée, le au moins un moteur (140) de fusée étant conçu pour recevoir le propergol (111) principal dans une plage de températures d'au moins approximativement plus que la température ambiante, afin de recevoir le propergol (121) secondaire du au moins un réservoir (120) de propergol secondaire dans une plage de températures d'au moins approximativement moins qu'une température ambiante; et faire réagir par voie exothermique les propergols (111, 121) principal et secondaire pour effectuer la combustion afin de fournir la poussée.
PCT/US2014/013247 2013-01-28 2014-01-27 Procédés et systèmes améliorés de moteurs de fusée à combustion Ceased WO2014149184A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201361757695P 2013-01-28 2013-01-28
US61/757,695 2013-01-28

Publications (2)

Publication Number Publication Date
WO2014149184A2 WO2014149184A2 (fr) 2014-09-25
WO2014149184A3 true WO2014149184A3 (fr) 2014-12-24

Family

ID=51581593

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2014/013247 Ceased WO2014149184A2 (fr) 2013-01-28 2014-01-27 Procédés et systèmes améliorés de moteurs de fusée à combustion

Country Status (1)

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WO (1) WO2014149184A2 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11028802B2 (en) 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
US12006067B2 (en) * 2019-05-30 2024-06-11 Launch On Demand Corporation Launch on demand
CN114109651B (zh) * 2021-11-09 2023-05-05 宁波天擎航天科技有限公司 一种固态燃料火箭组合冲压发动机
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
FR3139367A1 (fr) * 2022-09-02 2024-03-08 Marius Celette Moteur-fusée hybride autophage

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877504A (en) * 1954-08-02 1959-03-17 Phillips Petroleum Co Method of bonding propellant grain to metal case
WO1995033022A1 (fr) * 1994-05-31 1995-12-07 Orr William C Procedes et compositions pour combustion en phase vapeur
US5529264A (en) * 1994-02-18 1996-06-25 Lockheed Missiles & Space Company, Inc. Launch vehicle system
US5765361A (en) * 1996-08-23 1998-06-16 Jones; Herbert Stephen Hybrid-LO2-LH2 low cost launch vehicle
WO2002074622A1 (fr) * 2001-03-16 2002-09-26 Lockheed Martin Corporation Moteur de fusee a poussee reduite et systeme d'event a etages
US20030098107A1 (en) * 1998-07-22 2003-05-29 M. Arif Karabeyoglu High regression rate hybrid rocket propellants and method of selecting
US20050081508A1 (en) * 2002-09-13 2005-04-21 Edelman Raymond B. Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
US7254936B1 (en) * 2004-04-26 2007-08-14 Knight Andrew F Simple solid propellant rocket engine and super-staged rocket
US20080173004A1 (en) * 2006-04-20 2008-07-24 Combustion Propulsion & Ballistic Technology Corp. Bi-propellant rocket motor having controlled thermal management
US8047472B1 (en) * 2006-06-06 2011-11-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ram booster

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2877504A (en) * 1954-08-02 1959-03-17 Phillips Petroleum Co Method of bonding propellant grain to metal case
US5529264A (en) * 1994-02-18 1996-06-25 Lockheed Missiles & Space Company, Inc. Launch vehicle system
WO1995033022A1 (fr) * 1994-05-31 1995-12-07 Orr William C Procedes et compositions pour combustion en phase vapeur
US5765361A (en) * 1996-08-23 1998-06-16 Jones; Herbert Stephen Hybrid-LO2-LH2 low cost launch vehicle
US20030098107A1 (en) * 1998-07-22 2003-05-29 M. Arif Karabeyoglu High regression rate hybrid rocket propellants and method of selecting
WO2002074622A1 (fr) * 2001-03-16 2002-09-26 Lockheed Martin Corporation Moteur de fusee a poussee reduite et systeme d'event a etages
US20050081508A1 (en) * 2002-09-13 2005-04-21 Edelman Raymond B. Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
US7254936B1 (en) * 2004-04-26 2007-08-14 Knight Andrew F Simple solid propellant rocket engine and super-staged rocket
US20080173004A1 (en) * 2006-04-20 2008-07-24 Combustion Propulsion & Ballistic Technology Corp. Bi-propellant rocket motor having controlled thermal management
US8047472B1 (en) * 2006-06-06 2011-11-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ram booster

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
BERGLUND ET AL.: "The United Launch Alliance Delta IV Vehicle -- An Update to the Pulse Settling Propellant Management Approach", PROGRESS IN PROPULSION PHYSICS, vol. 1, 2009, pages 293 - 304 *
ZHENG ET AL.: "LM-3A Series Launch Vehicle User's Manual", PAYLOAD FAIRING, 2011, pages 1 - 254, Retrieved from the Internet <URL:http://cn.cgwic.com/LaunchServices/Download/manual/LM-3A%20Series%20Launch%20Vehicles%20User's%20Manual%20Issue%202011.pdf> [retrieved on 20141015] *

Also Published As

Publication number Publication date
WO2014149184A2 (fr) 2014-09-25

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