FR1336660A - Rocket propulsion device using solid propellant - Google Patents

Rocket propulsion device using solid propellant

Info

Publication number
FR1336660A
FR1336660A FR823698A FR823698A FR1336660A FR 1336660 A FR1336660 A FR 1336660A FR 823698 A FR823698 A FR 823698A FR 823698 A FR823698 A FR 823698A FR 1336660 A FR1336660 A FR 1336660A
Authority
FR
France
Prior art keywords
propulsion device
solid propellant
rocket propulsion
rocket
propellant
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
FR823698A
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.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel AG
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 to NL106643D priority Critical patent/NL106643C/xx
Priority to NL250244D priority patent/NL250244A/xx
Priority to DEK37426A priority patent/DE1153942B/en
Application filed by Dynamit Nobel AG filed Critical Dynamit Nobel AG
Priority to FR823698A priority patent/FR1336660A/en
Application granted granted Critical
Publication of FR1336660A publication Critical patent/FR1336660A/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
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/12Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • 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
    • 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
    • F02K9/36Propellant charge supports
    • 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
    • F02K9/97Rocket nozzles
    • 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
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR823698A 1959-04-08 1960-04-07 Rocket propulsion device using solid propellant Expired FR1336660A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
NL106643D NL106643C (en) 1960-04-07
NL250244D NL250244A (en) 1960-04-07
DEK37426A DE1153942B (en) 1959-04-08 1959-04-08 Solid propellant rocket
FR823698A FR1336660A (en) 1960-04-07 1960-04-07 Rocket propulsion device using solid propellant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR823698A FR1336660A (en) 1960-04-07 1960-04-07 Rocket propulsion device using solid propellant

Publications (1)

Publication Number Publication Date
FR1336660A true FR1336660A (en) 1963-09-06

Family

ID=8728851

Family Applications (1)

Application Number Title Priority Date Filing Date
FR823698A Expired FR1336660A (en) 1959-04-08 1960-04-07 Rocket propulsion device using solid propellant

Country Status (2)

Country Link
FR (1) FR1336660A (en)
NL (2) NL106643C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2473630A1 (en) * 1979-11-30 1981-07-17 Messerschmitt Boelkow Blohm TAPERING TUBE FOR REACTION ENGINES, PARTICULARLY FOR STATO-REACTORS OF FLANGES
DE4018794C2 (en) * 1989-06-15 2000-06-08 Poudres Et Explosifs Paris Soc Engine with a Propergolblock, which is provided with a central channel with a variable cross-section

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2473630A1 (en) * 1979-11-30 1981-07-17 Messerschmitt Boelkow Blohm TAPERING TUBE FOR REACTION ENGINES, PARTICULARLY FOR STATO-REACTORS OF FLANGES
DE4018794C2 (en) * 1989-06-15 2000-06-08 Poudres Et Explosifs Paris Soc Engine with a Propergolblock, which is provided with a central channel with a variable cross-section

Also Published As

Publication number Publication date
NL250244A (en)
NL106643C (en)

Similar Documents

Publication Publication Date Title
BE598253A (en) Thrust reverser device
FR1281397A (en) Development of rocket thrusters
CH379967A (en) rocket
CH400838A (en) Rocket launcher
BE601544A (en) Rocket
FR75318E (en) Rocket safety device
FR1330218A (en) Nautical propulsion device
FR1336660A (en) Rocket propulsion device using solid propellant
FR1265327A (en) Ignition device of the cruising thruster of a self-propelled projectile
CH375176A (en) Thrust booster on jet engine
FR1274839A (en) Rocket device
FR1270328A (en) Rocket propelled projectile
FR1273933A (en) Safety device for rocket nozzle
FR1286537A (en) Marine rocket
FR1250223A (en) Cargo ship
FR1257490A (en) Rocket for projectiles
BE604238A (en) Recoil-free gun propellant charge
FR1240629A (en) Nautical thruster
FR1276441A (en) Rocket engine using two liquid propellants
BE597023A (en) Propellant charge.
FR1293544A (en) Rocket propellant charge
DK102011C (en) Reaction engine for propelling boats.
CH382600A (en) Explosive weapon intended for training purposes
FR1345443A (en) solid fuel rocket propulsion equipment
FR1279419A (en) Rocket engine