JP2011515614A5 - - Google Patents

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Publication number
JP2011515614A5
JP2011515614A5 JP2011500828A JP2011500828A JP2011515614A5 JP 2011515614 A5 JP2011515614 A5 JP 2011515614A5 JP 2011500828 A JP2011500828 A JP 2011500828A JP 2011500828 A JP2011500828 A JP 2011500828A JP 2011515614 A5 JP2011515614 A5 JP 2011515614A5
Authority
JP
Japan
Prior art keywords
propellant
combustion
pellets
rocket motor
solid fuel
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.)
Granted
Application number
JP2011500828A
Other languages
English (en)
Japanese (ja)
Other versions
JP5016134B2 (ja
JP2011515614A (ja
Filing date
Publication date
Priority claimed from US12/053,475 external-priority patent/US7685940B1/en
Application filed filed Critical
Publication of JP2011515614A publication Critical patent/JP2011515614A/ja
Publication of JP2011515614A5 publication Critical patent/JP2011515614A5/ja
Application granted granted Critical
Publication of JP5016134B2 publication Critical patent/JP5016134B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011500828A 2008-03-21 2009-02-10 ペレットと塊状の固体推進剤とを持つロケットモータ Active JP5016134B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/053,475 US7685940B1 (en) 2008-03-21 2008-03-21 Rocket motor with pellet and bulk solid propellants
US12/053,475 2008-03-21
PCT/US2009/033694 WO2009134510A2 (en) 2008-03-21 2009-02-10 Rocket motor with pellet and bulk solid propellants

Publications (3)

Publication Number Publication Date
JP2011515614A JP2011515614A (ja) 2011-05-19
JP2011515614A5 true JP2011515614A5 (enExample) 2012-01-26
JP5016134B2 JP5016134B2 (ja) 2012-09-05

Family

ID=41255646

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011500828A Active JP5016134B2 (ja) 2008-03-21 2009-02-10 ペレットと塊状の固体推進剤とを持つロケットモータ

Country Status (4)

Country Link
US (1) US7685940B1 (enExample)
EP (1) EP2281114B1 (enExample)
JP (1) JP5016134B2 (enExample)
WO (1) WO2009134510A2 (enExample)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090000268A1 (en) * 2007-03-20 2009-01-01 Yurash Greg J Thermonuclear plasma reactor for rocket thrust and electrical generation
US8127534B2 (en) * 2008-02-19 2012-03-06 Raytheon Company Pellet loaded attitude control rocket motor
US20100011742A1 (en) * 2008-07-17 2010-01-21 Cavalleri Robert J Rocket Motor Containing Multiple Pellet Cells
US8242422B2 (en) * 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system
US8667776B2 (en) 2009-02-23 2014-03-11 Raytheon Company Pellet-loaded multiple impulse rocket motor
US20110024165A1 (en) * 2009-07-31 2011-02-03 Raytheon Company Systems and methods for composite structures with embedded interconnects
US8713912B2 (en) * 2010-07-12 2014-05-06 Raytheon Company Solid propellant rocket motors employing tungsten alloy burst discs and methods for the manufacture thereof
US8826640B2 (en) 2010-11-12 2014-09-09 Raytheon Company Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof
US20120304620A1 (en) * 2011-06-01 2012-12-06 Aerojet-General Corporation Catalyst, gas generator, and thruster with improved thermal capability and corrosion resistance
US8683933B1 (en) 2012-01-29 2014-04-01 Mario Placido Portela Solid rocket braking system
FR2995364A1 (fr) * 2012-09-13 2014-03-14 Astrium Sas Dispositif de propulsion hybride anaerobie a carburant presente sous de forme de solides divises
CN104747319B (zh) * 2014-01-01 2019-05-21 冯石文 一种固体燃料火箭发动机
US10563617B2 (en) * 2016-09-23 2020-02-18 Raytheon Company Electrically operated propellant for solid rocket motor thrust management
ES2901239T3 (es) * 2018-12-10 2022-03-21 Tecnesis 3000 Sl Dispositivo de energía con base en la reacción de álcali-agua
CN114060168B (zh) * 2021-11-05 2024-01-19 江西洪都航空工业集团有限责任公司 一种大初始推力端燃装药固体火箭发动机
CN115559829B (zh) * 2022-10-28 2024-07-12 中北大学 一种可重复装填多脉冲固体火箭发动机

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US6968676B1 (en) * 2001-11-01 2005-11-29 Krishnan Vinu B Propulsion from combustion of solid propellant pellet-projectiles
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US7194852B1 (en) * 2005-01-07 2007-03-27 Krishnan Vinu B Propulsion from combustion of solid propellant pellet-projectiles

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