BE617315A - Moteur-fusée - Google Patents

Moteur-fusée

Info

Publication number
BE617315A
BE617315A BE617315A BE617315A BE617315A BE 617315 A BE617315 A BE 617315A BE 617315 A BE617315 A BE 617315A BE 617315 A BE617315 A BE 617315A BE 617315 A BE617315 A BE 617315A
Authority
BE
Belgium
Prior art keywords
rocket engine
rocket
engine
Prior art date
Application number
BE617315A
Other languages
English (en)
Inventor
John Henry Grover
James Reeve Macpherson
Original Assignee
Atlantic Res Corp
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 Atlantic Res Corp filed Critical Atlantic Res Corp
Publication of BE617315A publication Critical patent/BE617315A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/70Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Liquid Carbonaceous Fuels (AREA)
  • Testing Of Engines (AREA)
BE617315A 1961-05-19 1962-05-07 Moteur-fusée BE617315A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US111396A US3122884A (en) 1961-05-19 1961-05-19 Rocket motor

Publications (1)

Publication Number Publication Date
BE617315A true BE617315A (fr) 1962-08-31

Family

ID=22338305

Family Applications (1)

Application Number Title Priority Date Filing Date
BE617315A BE617315A (fr) 1961-05-19 1962-05-07 Moteur-fusée

Country Status (3)

Country Link
US (1) US3122884A (fr)
BE (1) BE617315A (fr)
GB (1) GB972723A (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3421325A (en) * 1961-11-08 1969-01-14 Joseph G Thibodaux Jr Solid propellant rocket motor
FR1327090A (fr) * 1962-03-20 1963-05-17 Snecma Perfectionnement aux propulseurs à plusieurs tuyères de réaction
US3253407A (en) * 1962-10-19 1966-05-31 Thiokol Chemical Corp Rocket motor and flow control insert therefor
US3269113A (en) * 1962-12-18 1966-08-30 Aerojet General Co Rocket motor having solid fuel insulating means
US3218798A (en) * 1963-01-30 1965-11-23 Atlantic Res Corp Spherical booster
US3300142A (en) * 1963-06-25 1967-01-24 Whittaker Corp Rocket nozzle capable of inducing flow separation
US3293855A (en) * 1963-10-16 1966-12-27 Gen Motors Corp Reignitable rocket
BE657225A (fr) * 1964-12-16
US3555958A (en) * 1965-05-05 1971-01-19 Hercules Inc Method for the manufacture of a rocket motor
DE1926378B1 (de) * 1969-05-23 1970-12-03 Messerschmitt Boelkow Blohm Brennkammer,insbesondere fuer Raketentriebwerke
US3942443A (en) * 1970-07-20 1976-03-09 Thiokol Corporation Rocket assisted projectile
US3908364A (en) * 1973-01-19 1975-09-30 United Technologies Corp Putty propellant stress refief system
GB2143514B (en) * 1978-04-21 1985-10-09 Rheinmetall Gmbh Liquid propulsive charge
JP3231778B2 (ja) * 1994-04-29 2001-11-26 コーダント・テクノロジーズ・インコーポレーテッド 固体推進薬の2パルスロケットモータが充填されたケース及び発火装置並びにその製造方法
US7150232B1 (en) 2001-05-25 2006-12-19 Omnitek Partners Llc Methods and apparatus for increasing aerodynamic performance of projectiles
US6727485B2 (en) * 2001-05-25 2004-04-27 Omnitek Partners Llc Methods and apparatus for increasing aerodynamic performance of projectiles
US7281367B2 (en) * 2003-12-05 2007-10-16 Alliant Techsystems Inc. Steerable, intermittently operable rocket propulsion system
US8156867B2 (en) * 2006-07-17 2012-04-17 Raytheon Company Methods and apparatus for multiple part missile
US8667776B2 (en) * 2009-02-23 2014-03-11 Raytheon Company Pellet-loaded multiple impulse rocket motor
US8350201B2 (en) 2010-10-14 2013-01-08 Raytheon Company Systems, apparatus and methods to compensate for roll orientation variations in missile components
RU2622141C1 (ru) * 2016-02-11 2017-06-13 Публичное акционерное общество Научно-производственное объединение "Искра" Ракетный двигатель твёрдого топлива
WO2018186923A2 (fr) 2017-01-16 2018-10-11 Spectre Enterprises, Inc. Agent propulsif
US11112222B2 (en) 2019-01-21 2021-09-07 Spectre Materials Sciences, Inc. Propellant with pattern-controlled burn rate
WO2022178007A1 (fr) 2021-02-16 2022-08-25 Spectre Materials Sciences, Inc. Amorce pour armes à feu et autres munitions

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US826293A (en) * 1903-12-10 1906-07-17 Wilhelm Theodor Unge Propelling charge for air-torpedoes, &c.
US1879579A (en) * 1929-10-25 1932-09-27 Karl Pohl Rocket
BE408330A (fr) * 1935-03-09
US2814179A (en) * 1953-05-08 1957-11-26 Leonard B Edelman Return burning motor
US2816721A (en) * 1953-09-15 1957-12-17 Taylor Richard John Rocket powered aerial vehicle
US2988879A (en) * 1958-11-24 1961-06-20 Thompson Ramo Wooldridge Inc Rocket with fluid flame extinguisher for extruded fuel
US2971097A (en) * 1959-01-02 1961-02-07 Thompson Ramo Wooldridge Inc Control for a semi-solid monofuel driven turboalternator and pump system

Also Published As

Publication number Publication date
GB972723A (en) 1964-10-14
US3122884A (en) 1964-03-03

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