FR1483473A - Solid internal combustion charge for rocket engines - Google Patents

Solid internal combustion charge for rocket engines

Info

Publication number
FR1483473A
FR1483473A FR65676A FR65676A FR1483473A FR 1483473 A FR1483473 A FR 1483473A FR 65676 A FR65676 A FR 65676A FR 65676 A FR65676 A FR 65676A FR 1483473 A FR1483473 A FR 1483473A
Authority
FR
France
Prior art keywords
internal combustion
rocket engines
solid internal
combustion charge
charge
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
FR65676A
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
Application filed by Dynamit Nobel AG filed Critical Dynamit Nobel AG
Priority to FR65676A priority Critical patent/FR1483473A/en
Application granted granted Critical
Publication of FR1483473A publication Critical patent/FR1483473A/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
    • F02K9/10—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)
FR65676A 1965-06-16 1966-06-15 Solid internal combustion charge for rocket engines Expired FR1483473A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR65676A FR1483473A (en) 1965-06-16 1966-06-15 Solid internal combustion charge for rocket engines

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DED0047516 1965-06-16
DED0047515 1965-06-16
FR65676A FR1483473A (en) 1965-06-16 1966-06-15 Solid internal combustion charge for rocket engines

Publications (1)

Publication Number Publication Date
FR1483473A true FR1483473A (en) 1967-06-02

Family

ID=27209837

Family Applications (1)

Application Number Title Priority Date Filing Date
FR65676A Expired FR1483473A (en) 1965-06-16 1966-06-15 Solid internal combustion charge for rocket engines

Country Status (1)

Country Link
FR (1) FR1483473A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4275657A (en) * 1976-12-30 1981-06-30 Societe Nationale Des Poudres Et Explosifs Spirally wound pyrotechnic charge useful for the propulsion of an engine and the like
FR2500149A1 (en) * 1981-02-17 1982-08-20 Poudres & Explosifs Ste Nale BULGARIAN BULK CHANNEL PROPULSIVE LOAD COMPRISING A STAR SECTION

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4275657A (en) * 1976-12-30 1981-06-30 Societe Nationale Des Poudres Et Explosifs Spirally wound pyrotechnic charge useful for the propulsion of an engine and the like
FR2500149A1 (en) * 1981-02-17 1982-08-20 Poudres & Explosifs Ste Nale BULGARIAN BULK CHANNEL PROPULSIVE LOAD COMPRISING A STAR SECTION
EP0059142A1 (en) * 1981-02-17 1982-09-01 Societe Nationale Des Poudres Et Explosifs Solid propellant charge having two thrust ranges having a central channel and a star-shaped section

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