FR1257399A - Solid fuel fuze comprising a combustion rate adjustment mechanism - Google Patents

Solid fuel fuze comprising a combustion rate adjustment mechanism

Info

Publication number
FR1257399A
FR1257399A FR827444A FR827444A FR1257399A FR 1257399 A FR1257399 A FR 1257399A FR 827444 A FR827444 A FR 827444A FR 827444 A FR827444 A FR 827444A FR 1257399 A FR1257399 A FR 1257399A
Authority
FR
France
Prior art keywords
fuze
adjustment mechanism
solid fuel
rate adjustment
combustion rate
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
FR827444A
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 Aircraft 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 US813805A external-priority patent/US3031842A/en
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Priority to FR827444A priority Critical patent/FR1257399A/en
Application granted granted Critical
Publication of FR1257399A publication Critical patent/FR1257399A/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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
    • 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
    • F02K9/26—Burning control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR827444A 1959-05-18 1960-05-17 Solid fuel fuze comprising a combustion rate adjustment mechanism Expired FR1257399A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR827444A FR1257399A (en) 1959-05-18 1960-05-17 Solid fuel fuze comprising a combustion rate adjustment mechanism

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US813805A US3031842A (en) 1959-05-18 1959-05-18 Thrust control for solid rocket
FR827444A FR1257399A (en) 1959-05-18 1960-05-17 Solid fuel fuze comprising a combustion rate adjustment mechanism

Publications (1)

Publication Number Publication Date
FR1257399A true FR1257399A (en) 1961-03-31

Family

ID=26186060

Family Applications (1)

Application Number Title Priority Date Filing Date
FR827444A Expired FR1257399A (en) 1959-05-18 1960-05-17 Solid fuel fuze comprising a combustion rate adjustment mechanism

Country Status (1)

Country Link
FR (1) FR1257399A (en)

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