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GB2028981B - Propellant block - Google Patents

Propellant block

Info

Publication number
GB2028981B
GB2028981B GB7923206A GB7923206A GB2028981B GB 2028981 B GB2028981 B GB 2028981B GB 7923206 A GB7923206 A GB 7923206A GB 7923206 A GB7923206 A GB 7923206A GB 2028981 B GB2028981 B GB 2028981B
Authority
GB
United Kingdom
Prior art keywords
propellant block
propellant
block
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
GB7923206A
Other versions
GB2028981A (en
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 Nationale des Poudres et Explosifs
Original Assignee
Societe Nationale des Poudres et Explosifs
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 Nationale des Poudres et Explosifs filed Critical Societe Nationale des Poudres et Explosifs
Publication of GB2028981A publication Critical patent/GB2028981A/en
Application granted granted Critical
Publication of GB2028981B publication Critical patent/GB2028981B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/0823Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
    • F42C19/0826Primers or igniters for the initiation or the propellant charge in a cartridged ammunition comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators
    • 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
    • F02K9/95Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/12Primers; Detonators electric

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Air Bags (AREA)
GB7923206A 1978-07-19 1979-07-04 Propellant block Expired GB2028981B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7821455A FR2431675A1 (en) 1978-07-19 1978-07-19 FRONTAL COMBUSTION PYROTECHNIC LOADING COMPRISING AN INHIBITED LONGITUDINAL CHANNEL WHICH INCLUDES FIRE ELEMENTS

Publications (2)

Publication Number Publication Date
GB2028981A GB2028981A (en) 1980-03-12
GB2028981B true GB2028981B (en) 1982-06-16

Family

ID=9210924

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7923206A Expired GB2028981B (en) 1978-07-19 1979-07-04 Propellant block

Country Status (3)

Country Link
FR (1) FR2431675A1 (en)
GB (1) GB2028981B (en)
IT (1) IT1121004B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2160625A (en) * 1984-05-12 1985-12-24 Diehl Gmbh & Co A propelling charge for large-calibre weapons
RU2175399C2 (en) * 1999-07-29 2001-10-27 Южно-Российский государственный технический университет Method of control of rate of combustion of high-energy condensed system
RU2259495C2 (en) * 2003-10-16 2005-08-27 Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" Solid-propellant charge
US11530669B2 (en) 2020-09-11 2022-12-20 Raytheon Company Variable burn-rate solid rocket motor ignition method
CN112855385B (en) * 2021-01-08 2022-03-29 西安近代化学研究所 Charging structure suitable for low-temperature ignition

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3570364A (en) * 1961-11-08 1971-03-16 Joseph G Thibodaux Jr Method of making a solid propellant rocket motor
FR1336958A (en) * 1962-09-05 1963-09-06 Du Pont Ignition device for solid propellants
US3389659A (en) * 1966-04-05 1968-06-25 Thiokol Chemical Corp Ignition apparatus for rocket motors

Also Published As

Publication number Publication date
GB2028981A (en) 1980-03-12
IT7968473A0 (en) 1979-07-13
FR2431675A1 (en) 1980-02-15
FR2431675B1 (en) 1981-06-12
IT1121004B (en) 1986-03-26

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19980704