GB2233745B - Process for making solid propellant blocks incorporating heat conductors,and the blocks so obtained. - Google Patents

Process for making solid propellant blocks incorporating heat conductors,and the blocks so obtained.

Info

Publication number
GB2233745B
GB2233745B GB8426524A GB8426524A GB2233745B GB 2233745 B GB2233745 B GB 2233745B GB 8426524 A GB8426524 A GB 8426524A GB 8426524 A GB8426524 A GB 8426524A GB 2233745 B GB2233745 B GB 2233745B
Authority
GB
United Kingdom
Prior art keywords
blocks
solid propellant
heat conductors
making solid
incorporating heat
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 - Lifetime
Application number
GB8426524A
Other versions
GB2233745A (en
Inventor
Christian Desormeaux
Roger Mespoulede
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 GB2233745A publication Critical patent/GB2233745A/en
Application granted granted Critical
Publication of GB2233745B publication Critical patent/GB2233745B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
    • C06B21/0033—Shaping the mixture
    • C06B21/0058—Shaping the mixture by casting a curable composition, e.g. of the plastisol type
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • 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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/22—Shape or structure of solid propellant charges of the front-burning type
    • 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
    • F02K9/24—Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
    • 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)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Continuous Casting (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Non-Insulated Conductors (AREA)
GB8426524A 1983-10-26 1984-10-19 Process for making solid propellant blocks incorporating heat conductors,and the blocks so obtained. Expired - Lifetime GB2233745B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8317044A FR2640259B1 (en) 1983-10-26 1983-10-26 METHOD OF MANUFACTURING BY MOLDING A BLOCK OF FRONTAL COMBUSTION SOLID PROPERGOL DRIVEN BY HEAT CONDUCTORS AND BLOCK OBTAINED BY THIS PROCESS

Publications (2)

Publication Number Publication Date
GB2233745A GB2233745A (en) 1991-01-16
GB2233745B true GB2233745B (en) 1991-07-31

Family

ID=9293535

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8426524A Expired - Lifetime GB2233745B (en) 1983-10-26 1984-10-19 Process for making solid propellant blocks incorporating heat conductors,and the blocks so obtained.

Country Status (4)

Country Link
DE (1) DE3438993A1 (en)
FR (1) FR2640259B1 (en)
GB (1) GB2233745B (en)
IT (1) IT1224139B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2776656B1 (en) * 1998-03-30 2000-04-28 Giat Ind Sa METHOD FOR MANUFACTURING AN OBJECT FROM A GRANULAR MATERIAL, IGNITION TUBE AND PROPULSIVE CHARGE OBTAINED WITH SUCH A METHOD
AU1323401A (en) * 1999-11-23 2001-06-04 Technanogy, Llc End-burning rocket motor
RU2607223C1 (en) * 2015-07-20 2017-01-10 Акционерное общество "Федеральный научно-производственный центр "Алтай" Method of making composite solid rocket propellant charge
RU2657077C1 (en) * 2016-03-31 2018-06-08 Акционерное общество "Федеральный научно-производственный центр "Алтай" Combined with the charge body mixed solid rocket fuel manufacturing method by the free-casting
CN109723575B (en) * 2018-11-26 2021-07-02 西安现代控制技术研究所 Tubular charging free-filling mode and method for realizing multi-thrust scheme
CN109973245B (en) * 2019-03-07 2020-07-14 北京灵动飞天动力科技有限公司 End-burning medicine embedded with composite metal wire
US11746728B1 (en) * 2022-03-31 2023-09-05 Raytheon Company Propulsion system with grooved inert rods for reactive wire

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3509822A (en) * 1960-06-09 1970-05-05 Susquehanna Corp Propellent grains
FR1349125A (en) * 1961-09-26 1964-01-17 Atlantic Res Corp Improvements to propellants
FR1603394A (en) * 1968-10-15 1971-04-13

Also Published As

Publication number Publication date
DE3438993C2 (en) 1992-09-17
GB2233745A (en) 1991-01-16
FR2640259A1 (en) 1990-06-15
IT1224139B (en) 1990-09-26
IT8468028A0 (en) 1984-10-17
DE3438993A1 (en) 1990-10-31
FR2640259B1 (en) 1992-01-03

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Legal Events

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

Effective date: 19961019