ES2822133T3 - Método de fabricación de un propulsor de cohete - Google Patents

Método de fabricación de un propulsor de cohete Download PDF

Info

Publication number
ES2822133T3
ES2822133T3 ES11840828T ES11840828T ES2822133T3 ES 2822133 T3 ES2822133 T3 ES 2822133T3 ES 11840828 T ES11840828 T ES 11840828T ES 11840828 T ES11840828 T ES 11840828T ES 2822133 T3 ES2822133 T3 ES 2822133T3
Authority
ES
Spain
Prior art keywords
propellant
hydrocarbon fluids
formulated
astm
weight
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.)
Active
Application number
ES11840828T
Other languages
English (en)
Spanish (es)
Inventor
Kevin Kelly
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.)
TotalEnergies Marketing Services SA
Original Assignee
Total Marketing Services SA
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
Priority claimed from US12/949,980 external-priority patent/US8574322B2/en
Application filed by Total Marketing Services SA filed Critical Total Marketing Services SA
Application granted granted Critical
Publication of ES2822133T3 publication Critical patent/ES2822133T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
    • 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
  • Liquid Carbonaceous Fuels (AREA)
ES11840828T 2010-11-19 2011-11-17 Método de fabricación de un propulsor de cohete Active ES2822133T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/949,980 US8574322B2 (en) 2010-11-19 2010-11-19 Propellant compositions and methods of making and using the same
US13/295,268 US20120124897A1 (en) 2010-11-19 2011-11-14 Propellant Compositions and Methods of Making and Using the Same
PCT/US2011/061181 WO2012068369A1 (en) 2010-11-19 2011-11-17 Propellant compositions and methods of making and using the same

Publications (1)

Publication Number Publication Date
ES2822133T3 true ES2822133T3 (es) 2021-04-29

Family

ID=46062990

Family Applications (1)

Application Number Title Priority Date Filing Date
ES11840828T Active ES2822133T3 (es) 2010-11-19 2011-11-17 Método de fabricación de un propulsor de cohete

Country Status (9)

Country Link
US (1) US20120124897A1 (enExample)
EP (1) EP2640953B1 (enExample)
JP (1) JP5914511B2 (enExample)
KR (1) KR101831218B1 (enExample)
CN (1) CN103282635B (enExample)
ES (1) ES2822133T3 (enExample)
IL (1) IL226174A0 (enExample)
TW (1) TW201235331A (enExample)
WO (1) WO2012068369A1 (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130220882A1 (en) * 2012-02-29 2013-08-29 Total Raffinage Marketing Jet Turbine Fuel Compositions and Methods of Making and Using the Same
US10065900B2 (en) 2015-06-02 2018-09-04 Johann Haltermann Limited High volumetric energy density rocket propellant
EP3315590A1 (en) * 2016-10-27 2018-05-02 Total Marketing Services Use of hydrocarbon fluids in electric vehicles
EP3315586A1 (en) * 2016-10-27 2018-05-02 Total Marketing Services Use of biodegradable hydrocarbon fluids as heat-transfer media
WO2021136757A1 (en) * 2019-12-30 2021-07-08 Shell Internationale Research Maatschappij B.V. Compositions and methods of producing rocket propellants with enhanced cryogenic cooling, thermal stability, and thrust efficiency performance

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3153903A (en) * 1961-04-04 1964-10-27 Jacques C Morrell Lithium rocket propellants and process for using the same
US3660183A (en) * 1961-12-27 1972-05-02 Texaco Inc Stable suspensions
JPS60118686A (ja) * 1983-11-28 1985-06-26 日本石油化学株式会社 高密度液体燃料
JPS62197492A (ja) * 1986-02-24 1987-09-01 Nippon Oil Co Ltd 高密度液体燃料
US5705771A (en) * 1990-10-29 1998-01-06 Flynn; Thomas M. Cryogenic propellants and method for producing cryogenic propellants
US5616882A (en) * 1994-12-09 1997-04-01 The United States Of America As Represented By The Secretary Of The Air Force High energy rocket propellant
EP1481038B1 (en) 2002-03-06 2013-08-14 ExxonMobil Chemical Patents Inc. Improved hydrocarbon fluids
EP1342774A1 (en) 2002-03-06 2003-09-10 ExxonMobil Chemical Patents Inc. A process for the production of hydrocarbon fluids
CN1860208A (zh) * 2003-08-01 2006-11-08 宝洁公司 用于喷气机、燃气轮机、火箭和柴油发动机的燃料
WO2005019392A2 (en) * 2003-08-01 2005-03-03 The Procter & Gamble Company Fuel for jet, gas turbine, rocket, and diesel engines
MX2011002831A (es) * 2008-09-17 2011-04-21 Amyris Biotechnologies Inc Composiciones de combustible que comprenden limoneno y farneseno.

Also Published As

Publication number Publication date
CN103282635A (zh) 2013-09-04
EP2640953A4 (en) 2017-08-16
WO2012068369A1 (en) 2012-05-24
EP2640953B1 (en) 2020-07-08
JP5914511B2 (ja) 2016-05-11
IL226174A0 (en) 2013-07-31
TW201235331A (en) 2012-09-01
JP2013545843A (ja) 2013-12-26
KR101831218B1 (ko) 2018-02-22
CN103282635B (zh) 2017-06-23
US20120124897A1 (en) 2012-05-24
KR20140042765A (ko) 2014-04-07
EP2640953A1 (en) 2013-09-25

Similar Documents

Publication Publication Date Title
ES2822133T3 (es) Método de fabricación de un propulsor de cohete
Manigandan et al. Impact of additives in Jet-A fuel blends on combustion, emission and exergetic analysis using a micro-gas turbine engine
Smith et al. Improvements in the measurement of distillation curves. 4. Application to the aviation turbine fuel Jet-A
Westbrook Biofuels combustion
DeLuca et al. Characterization of HTPB-based solid fuel formulations: Performance, mechanical properties, and pollution
US9005380B2 (en) High performance liquid rocket propellant
Luning Prak et al. Densities, viscosities, speeds of sound, bulk moduli, surface tensions, and flash points of binary mixtures of ethylcyclohexane or methylcyclohexane with n-dodecane or n-hexadecane at 0.1 MPa
Xue et al. The blending effect on the sooting tendencies of alternative/conventional jet fuel blends in non-premixed flames
NO344850B1 (no) Drivstoffblanding som inneholder en Fischer-Tropsch-avledet drivstoffkomponent
Cai et al. Effect of grain port length–diameter ratio on combustion performance in hybrid rocket motors
Mahottamananda et al. Regression Rate Characterization of HTPB‐Paraffin Based Solid Fuels for Hybrid Rocket
Li et al. Densities and viscosities for the ternary system of (ethylcyclohexane+ 1-butanol+ ethyl octanoate) and corresponding binary systems at T=(293.15–323.15) K
Kuyucu et al. Investigation of the effect of biofuel addition to jet fuel on engine performance and emissions in model jet engine
Basha et al. An emission control strategy in a low capacity single cylinder compression ignition engine powered with DEE blended fuels
US8574322B2 (en) Propellant compositions and methods of making and using the same
Blakey et al. Fuel effects on range versus payload for modern jet aircraft
García-Contreras et al. Biojet fuels and emissions
Wang Kinetic mechanism of surrogates for biodiesel
Saleh et al. Study of the flame characteristics of biodiesel blend fuel in a semi-industrial boiler
US3177653A (en) High mach number jet fuel comprising polycyclic hydrocarbons and isoparaffinic hydrocarbons
WO2013127799A2 (en) Jet turbine fuel compositions and methods of making and using the same
Wey et al. Effects of bio-derived fuels on emissions and performance using a 9-point lean direct injection low emissions concept
Sidhu et al. Evaporation and Flammability Studies of Jet A-1 Fuel Blended with n-hexane and Domestic Grade Kerosene
Jacoby Cool fuel for hypersonic aircraft
Bar-Kohany et al. Advances in Liquid Atomization via Flash Boiling—A Global Overview. Energies 2023, 16, 6763