FR2466627B1 - - Google Patents

Info

Publication number
FR2466627B1
FR2466627B1 FR7924867A FR7924867A FR2466627B1 FR 2466627 B1 FR2466627 B1 FR 2466627B1 FR 7924867 A FR7924867 A FR 7924867A FR 7924867 A FR7924867 A FR 7924867A FR 2466627 B1 FR2466627 B1 FR 2466627B1
Authority
FR
France
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
FR7924867A
Other languages
French (fr)
Other versions
FR2466627A1 (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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7924867A priority Critical patent/FR2466627A1/fr
Publication of FR2466627A1 publication Critical patent/FR2466627A1/fr
Application granted granted Critical
Publication of FR2466627B1 publication Critical patent/FR2466627B1/fr
Granted 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
    • F02K9/36—Propellant charge supports

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
FR7924867A 1979-10-05 1979-10-05 Dispositif anti-clappement pour propulseur a propergol solide Granted FR2466627A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7924867A FR2466627A1 (fr) 1979-10-05 1979-10-05 Dispositif anti-clappement pour propulseur a propergol solide

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7924867A FR2466627A1 (fr) 1979-10-05 1979-10-05 Dispositif anti-clappement pour propulseur a propergol solide

Publications (2)

Publication Number Publication Date
FR2466627A1 FR2466627A1 (fr) 1981-04-10
FR2466627B1 true FR2466627B1 (ref) 1983-08-19

Family

ID=9230374

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7924867A Granted FR2466627A1 (fr) 1979-10-05 1979-10-05 Dispositif anti-clappement pour propulseur a propergol solide

Country Status (1)

Country Link
FR (1) FR2466627A1 (ref)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2591281B1 (fr) * 1985-12-05 1988-04-01 Europ Propulsion Amenagement interne anti-clappement pour propulseur a poudre et son procede de fabrication.
RU2194875C1 (ru) * 2001-09-20 2002-12-20 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Устройство для формования зарядов из смесевого твердого топлива
RU2302546C2 (ru) * 2005-08-10 2007-07-10 Открытое акционерное общество Научно-производственное объединение "Искра" Корпус ракетного двигателя твердого топлива
RU2426000C1 (ru) * 2009-12-24 2011-08-10 Федеральное государственное унитарное предприятие "Федеральный центр двойных технологий "Союз" (ФГУП "ФЦДТ "Союз") Устройство для формования канального заряда из смесевого ракетного твердого топлива
RU2446307C1 (ru) * 2010-10-21 2012-03-27 Открытое акционерное общество Научно-производственное объединение "Искра" Ракетный двигатель твердого топлива
RU2459101C1 (ru) * 2011-02-21 2012-08-20 Открытое акционерное общество Научно-производственное объединение "Искра" Корпус ракетного двигателя твердого топлива и заряд скрепленный
RU2498101C2 (ru) * 2011-12-05 2013-11-10 Открытое акционерное общество Научно-производственное объединение "Искра" Снаряженный корпус ракетного двигателя твердого топлива
RU2635171C1 (ru) * 2016-12-06 2017-11-09 Публичное акционерное общество Научно-производственное объединение "Искра" Корпус ракетного двигателя твёрдого топлива
IT201700115681A1 (it) * 2017-10-13 2019-04-13 Avio Spa Procedimento di collaudo per collaudare un motore a propellente solido, e motore a propellente solido per attuare tale procedimento
CN114941584B (zh) * 2022-04-28 2025-09-30 湖北航天技术研究院总体设计所 适用于固体姿控发动机压强波动的绝热结构及燃发器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2733568A (en) * 1956-02-07 Solid propellant jet reaction motor
US2957309A (en) * 1957-07-22 1960-10-25 Phillips Petroleum Co Rocket motor
US3616646A (en) * 1970-03-24 1971-11-02 Us Air Force Forward or aft stress relief for a case bonded solid propellant
JPS533445B2 (ref) * 1973-10-17 1978-02-07
US3919841A (en) * 1974-07-05 1975-11-18 Us Navy Rocket motor apparatus

Also Published As

Publication number Publication date
FR2466627A1 (fr) 1981-04-10

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Legal Events

Date Code Title Description
ST Notification of lapse