GB1085177A - Improvements in rocket projectiles having a war-head - Google Patents

Improvements in rocket projectiles having a war-head

Info

Publication number
GB1085177A
GB1085177A GB2684965A GB2684965A GB1085177A GB 1085177 A GB1085177 A GB 1085177A GB 2684965 A GB2684965 A GB 2684965A GB 2684965 A GB2684965 A GB 2684965A GB 1085177 A GB1085177 A GB 1085177A
Authority
GB
United Kingdom
Prior art keywords
casing
bore
diaphragm
charge
war
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
GB2684965A
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.)
Brevets Aero Mecaniques SA
Original Assignee
Brevets Aero Mecaniques 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 Brevets Aero Mecaniques SA filed Critical Brevets Aero Mecaniques SA
Publication of GB1085177A publication Critical patent/GB1085177A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes
    • F42C19/08—Primers; Detonators
    • F42C19/0819—Primers or igniters for the initiation of rocket motors, i.e. pyrotechnical aspects thereof
    • D—TEXTILES; PAPER
    • D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G1/00—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics
    • D02G1/14—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics using grooved rollers or gear-wheel-type members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes
    • F42C19/08—Primers; Detonators
    • F42C19/12—Primers; Detonators electric

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Elimination Of Static Electricity (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1,085,177. Self-propelled missiles. BREVETS AERO-MECANIQUES S.A. June 24, 1965 [June 27, 1964], No. 26849/65. Heading F3A A war rocket comprises a cylindrical motor 1 and a warhead 3 connected together by a threaded casing 4 housing ignition means for the propellant 2. In casing 4 is an annular recess filled with a primary charge 7 and closed by a thin diaphragm 11. An electric primer 8 for initiating the charge 7 is housed in a bore leading to the recess and connected by wires 5a to electric leads 5 which extend through the motor and emerge from the nozzle. A second bore 9 is used to introduce the charge 7 and is closed by a threaded plug 10 which can be removed for inspection purposes. Bore 9 extends longitudinally of the casing 4. Casing 4 may be made of light alloy and the diaphragm of aluminium or aluminium alloy. Diaphragm 11 may be glued in position. After inserting the primer 8, the front of the casing may be waterproofed, e.g. with a rubber solution.
GB2684965A 1964-06-27 1965-06-24 Improvements in rocket projectiles having a war-head Expired GB1085177A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
LU46409 1964-06-27

Publications (1)

Publication Number Publication Date
GB1085177A true GB1085177A (en) 1967-09-27

Family

ID=19723850

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2684965A Expired GB1085177A (en) 1964-06-27 1965-06-24 Improvements in rocket projectiles having a war-head

Country Status (9)

Country Link
BE (1) BE665731A (en)
CH (1) CH439018A (en)
DE (1) DE1453809A1 (en)
ES (1) ES314716A1 (en)
FR (1) FR1439475A (en)
GB (1) GB1085177A (en)
IL (1) IL23777A (en)
LU (1) LU46409A1 (en)
NL (1) NL6507840A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3808973A (en) * 1971-05-31 1974-05-07 Giulo Fiocchi Spa Self-propelling projectile for firearms
US4864817A (en) * 1983-05-26 1989-09-12 Morton Thiokol, Inc. Membrane seal for application to pulsed rocket motor

Also Published As

Publication number Publication date
DE1453809A1 (en) 1969-02-06
NL6507840A (en) 1965-12-28
LU46409A1 (en) 1972-01-01
CH63565A4 (en) 1967-12-15
CH439018A (en) 1967-12-15
ES314716A1 (en) 1965-10-01
IL23777A (en) 1969-07-30
BE665731A (en) 1965-10-18
FR1439475A (en) 1966-05-20

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