FR1336660A - Dispositif de propulsion de fusées utilisant un propergol solide - Google Patents

Dispositif de propulsion de fusées utilisant un propergol solide

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
English (en)
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 NL250244D priority Critical patent/NL250244A/xx
Priority to NL106643D priority patent/NL106643C/xx
Priority to DEK37426A priority patent/DE1153942B/de
Application filed by Dynamit Nobel AG filed Critical Dynamit Nobel AG
Priority to FR823698A priority patent/FR1336660A/fr
Application granted granted Critical
Publication of FR1336660A publication Critical patent/FR1336660A/fr
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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • 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
    • 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
    • F02K9/36—Propellant charge supports
    • 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
    • F02K9/97—Rocket nozzles
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- 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 Dispositif de propulsion de fusées utilisant un propergol solide Expired FR1336660A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
NL250244D NL250244A (enrdf_load_stackoverflow) 1960-04-07
NL106643D NL106643C (enrdf_load_stackoverflow) 1960-04-07
DEK37426A DE1153942B (de) 1959-04-08 1959-04-08 Festtreibstoffrakete
FR823698A FR1336660A (fr) 1960-04-07 1960-04-07 Dispositif de propulsion de fusées utilisant un propergol solide

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR823698A FR1336660A (fr) 1960-04-07 1960-04-07 Dispositif de propulsion de fusées utilisant un propergol solide

Publications (1)

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

Family

ID=8728851

Family Applications (1)

Application Number Title Priority Date Filing Date
FR823698A Expired FR1336660A (fr) 1959-04-08 1960-04-07 Dispositif de propulsion de fusées utilisant un propergol solide

Country Status (2)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2473630A1 (fr) * 1979-11-30 1981-07-17 Messerschmitt Boelkow Blohm Tuyere de poussee de decollage pour moteurs a reaction, en particulier pour stato-reacteurs de fusees
DE4018794C2 (de) * 1989-06-15 2000-06-08 Poudres Et Explosifs Paris Soc Triebwerk mit einem Propergolblock, der mit einem Mittenkanal mit veränderlichem Querschnitt versehen ist

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2473630A1 (fr) * 1979-11-30 1981-07-17 Messerschmitt Boelkow Blohm Tuyere de poussee de decollage pour moteurs a reaction, en particulier pour stato-reacteurs de fusees
DE4018794C2 (de) * 1989-06-15 2000-06-08 Poudres Et Explosifs Paris Soc Triebwerk mit einem Propergolblock, der mit einem Mittenkanal mit veränderlichem Querschnitt versehen ist

Also Published As

Publication number Publication date
NL250244A (enrdf_load_stackoverflow)
NL106643C (enrdf_load_stackoverflow)

Similar Documents

Publication Publication Date Title
BE598253A (fr) Dispositif inverseur de poussée
FR1281397A (fr) Perfectionnement aux propulseurs pour fusées
CH379967A (de) Rakete
BE601544A (fr) Fusée
CH400838A (fr) Dispositif de lancement de fusée
FR75318E (fr) Dispositif de sécurité pour fusées
FR1330218A (fr) Dispositif de propulsion nautique
BE604238A (fr) Charge propulsive pour canons exempt de recul
FR1336660A (fr) Dispositif de propulsion de fusées utilisant un propergol solide
FR1265327A (fr) Dispositif d'allumage du propulseur de croisière d'un projectile autopropulsé
CH375176A (de) Schubverstärker an Strahltriebwerk
BE584189A (fr) Explosifs et agents de propulsion
FR1274839A (fr) Dispositif de fusée
FR1270328A (fr) Projectile propulsé par roquette
FR1196091A (fr) Dispositif lance-roquettes
FR1273933A (fr) Dispositif de sécurité pour tuyère de fusée
FR1286537A (fr) Fusée marine
FR1250223A (fr) Navire de charge
FR1257490A (fr) Fusée pour projectiles
FR1240629A (fr) Propulseur nautique
FR1276441A (fr) Moteur de fusée utilisant deux agents propulsifs liquides
BE597023A (fr) Charge propulsive.
FR1293544A (fr) Charge propulsive pour fusées
DK102011C (da) Reaktionsmotor til fremdrift af både.
CH382600A (de) Zu Übungszwecken bestimmte explosive Waffe