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.)
Raytheon Technologies 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

    • 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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/343—Joints, connections, seals therefor
    • 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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/18—Shape 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

Similar Documents

Publication Publication Date Title
BE590820A (en) Solid fuel rocket thrust regulator
FR1315914A (en) Engine for rockets or missiles of the multi-section or multi-element type and solid fuel
BE595366A (en) Swivel nozzle for solid fuel rocket.
FR1224153A (en) Solid fuel for rocket propulsion
FR1301955A (en) Combustion engine
FR1462157A (en) Improvements to internal combustion engines
FR1333377A (en) Scraper ring for internal combustion engine
FR1289248A (en) Reignition solid fuel rocket engine
BE611337A (en) Segmented solid fuel rocket engine.
FR1345443A (en) solid fuel rocket propulsion equipment
FR1281438A (en) Solid fuel mechanically loaded boiler
FR80003E (en) Container for storage and transport of combustion engine
FR1256287A (en) Acid neutralizer for internal combustion engines
FR1380465A (en) Solid fuel rocket arrangement
FR1305665A (en) Combustion engine
FR1295974A (en) Combustion engine
FR1317076A (en) Fuel injection pump for combustion engines
BE613168R (en) Rocket and explosives fuels
FR1313058A (en) New rocket fuels and combustion additives
FR1299060A (en) Improvements to internal combustion engines
FR1327220A (en) Enhancements to solid fuel rockets and multiple nozzles
FR1386870A (en) Solid fuel jet engine
FR1308423A (en) Rotary internal combustion engine
FR1280781A (en) Container for storage and transport of combustion engines
FR1312130A (en) Improvements to launchers for combustion engine starters