GB840257A - Improvements in rockets - Google Patents

Improvements in rockets

Info

Publication number
GB840257A
GB840257A GB26054/58A GB2605458A GB840257A GB 840257 A GB840257 A GB 840257A GB 26054/58 A GB26054/58 A GB 26054/58A GB 2605458 A GB2605458 A GB 2605458A GB 840257 A GB840257 A GB 840257A
Authority
GB
United Kingdom
Prior art keywords
rocket
aug
head
motor
weight
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
GB26054/58A
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 GB840257A publication Critical patent/GB840257A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Automatic Assembly (AREA)

Abstract

840,257. Self propelled missiles. BREVETS AERO-MECANIQUES S. A. Aug. 13, 1958 [Aug. 24, 1957], No. 26054/58. Class 9(2). Between the head 2 and the motor 1 of a missile are provided a number of chambers 3 into or from which explosive or inert ballast may be loaded or removed immediately before launching in order to vary the launching weight of the rocket. In another embodiment the weight of the rocket may be altered by varying the number of detachable sections 4 interposed between the head 2 and the motor 1.
GB26054/58A 1957-08-24 1958-08-13 Improvements in rockets Expired GB840257A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
LU840257X 1957-08-24

Publications (1)

Publication Number Publication Date
GB840257A true GB840257A (en) 1960-07-06

Family

ID=19734040

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26054/58A Expired GB840257A (en) 1957-08-24 1958-08-13 Improvements in rockets

Country Status (3)

Country Link
BE (1) BE570007A (en)
DE (1) DE1130735B (en)
GB (1) GB840257A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2343988A1 (en) * 1976-03-09 1977-10-07 Rheinmetall Gmbh COMBAT OR EXERCISE PROJECTILE
FR2475715A1 (en) * 1980-02-13 1981-08-14 Maurel Robert Modular element for sectional projectile - is stacked and made of synthetic injected material with slight clearance to aid stacking
FR2533687A1 (en) * 1982-09-27 1984-03-30 Meca Ste Nle Et Method of modular manufacture of fuses of various types for projectiles, and fuses produced according to this method as well as constructive elements for their manufacture.
SE2000094A1 (en) * 2020-05-22 2021-11-23 Bae Systems Bofors Ab Projectile

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR816083A (en) * 1936-03-30 1937-07-29 Projectile improvements
US2422720A (en) * 1944-08-15 1947-06-24 Carolus L Eksergian Rocket projectile

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2343988A1 (en) * 1976-03-09 1977-10-07 Rheinmetall Gmbh COMBAT OR EXERCISE PROJECTILE
FR2475715A1 (en) * 1980-02-13 1981-08-14 Maurel Robert Modular element for sectional projectile - is stacked and made of synthetic injected material with slight clearance to aid stacking
FR2533687A1 (en) * 1982-09-27 1984-03-30 Meca Ste Nle Et Method of modular manufacture of fuses of various types for projectiles, and fuses produced according to this method as well as constructive elements for their manufacture.
SE2000094A1 (en) * 2020-05-22 2021-11-23 Bae Systems Bofors Ab Projectile
WO2021235989A1 (en) * 2020-05-22 2021-11-25 Bae Systems Bofors Ab Short-range projectile
SE545006C2 (en) * 2020-05-22 2023-02-28 Bae Systems Bofors Ab Projectile

Also Published As

Publication number Publication date
BE570007A (en)
DE1130735B (en) 1962-05-30

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