FR1315914A - Engine for rockets or missiles of the multi-section or multi-element type and solid fuel - Google Patents

Engine for rockets or missiles of the multi-section or multi-element type and solid fuel

Info

Publication number
FR1315914A
FR1315914A FR881998A FR881998A FR1315914A FR 1315914 A FR1315914 A FR 1315914A FR 881998 A FR881998 A FR 881998A FR 881998 A FR881998 A FR 881998A FR 1315914 A FR1315914 A FR 1315914A
Authority
FR
France
Prior art keywords
rockets
missiles
engine
section
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.)
Expired
Application number
FR881998A
Other languages
French (fr)
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.)
RTX Corp
Original Assignee
United Technologies 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
Priority claimed from GB755661A external-priority patent/GB918936A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Priority to FR881998A priority Critical patent/FR1315914A/en
Application granted granted Critical
Publication of FR1315914A publication Critical patent/FR1315914A/en
Expired legal-status Critical Current

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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/343Joints, connections, seals therefor
    • 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/18Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR881998A 1961-03-01 1961-12-14 Engine for rockets or missiles of the multi-section or multi-element type and solid fuel Expired FR1315914A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR881998A FR1315914A (en) 1961-03-01 1961-12-14 Engine for rockets or missiles of the multi-section or multi-element type and solid fuel

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB755661A GB918936A (en) 1961-03-01 1961-03-01 Improvements in or relating to rocket motors
FR881998A FR1315914A (en) 1961-03-01 1961-12-14 Engine for rockets or missiles of the multi-section or multi-element type and solid fuel

Publications (1)

Publication Number Publication Date
FR1315914A true FR1315914A (en) 1963-01-25

Family

ID=26193522

Family Applications (1)

Application Number Title Priority Date Filing Date
FR881998A Expired FR1315914A (en) 1961-03-01 1961-12-14 Engine for rockets or missiles of the multi-section or multi-element type and solid fuel

Country Status (1)

Country Link
FR (1) FR1315914A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2461728C2 (en) * 2010-12-03 2012-09-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Solid-propellant rocket engine
WO2013019898A1 (en) * 2011-08-01 2013-02-07 The Aerospace Corporation Systems and methods for casting hybrid rocket motor fuel grains
US8601790B2 (en) 2008-02-28 2013-12-10 The Aerospace Corporation Buried radial flow rapid prototyping rocket motors
US8707676B2 (en) 2008-02-28 2014-04-29 The Aerospace Corporation Radial flow rapid prototyping rocket motors
US8844133B2 (en) 2008-02-28 2014-09-30 The Aerospace Corporation Stereolithographic rocket motor manufacturing method
US9038368B2 (en) 2011-08-01 2015-05-26 The Aerospace Corporation Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8601790B2 (en) 2008-02-28 2013-12-10 The Aerospace Corporation Buried radial flow rapid prototyping rocket motors
US8707676B2 (en) 2008-02-28 2014-04-29 The Aerospace Corporation Radial flow rapid prototyping rocket motors
US8844133B2 (en) 2008-02-28 2014-09-30 The Aerospace Corporation Stereolithographic rocket motor manufacturing method
RU2461728C2 (en) * 2010-12-03 2012-09-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Solid-propellant rocket engine
WO2013019898A1 (en) * 2011-08-01 2013-02-07 The Aerospace Corporation Systems and methods for casting hybrid rocket motor fuel grains
US9038368B2 (en) 2011-08-01 2015-05-26 The Aerospace Corporation Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor
US9429104B2 (en) 2011-08-01 2016-08-30 The Aerospace Corporation Systems and methods for casting hybrid rocket motor fuel grains

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