FR1363559A - Rocket projectile stabilized in rotation - Google Patents

Rocket projectile stabilized in rotation

Info

Publication number
FR1363559A
FR1363559A FR938892A FR938892A FR1363559A FR 1363559 A FR1363559 A FR 1363559A FR 938892 A FR938892 A FR 938892A FR 938892 A FR938892 A FR 938892A FR 1363559 A FR1363559 A FR 1363559A
Authority
FR
France
Prior art keywords
rotation
rocket projectile
projectile stabilized
stabilized
rocket
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
FR938892A
Other languages
French (fr)
Inventor
Karl-Otto Wehlow
Fritz Woyt
Hermann Renner
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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
Priority claimed from DER33038A external-priority patent/DE1213760B/en
Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Priority to FR938892A priority Critical patent/FR1363559A/en
Application granted granted Critical
Publication of FR1363559A publication Critical patent/FR1363559A/en
Expired 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
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/12—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge rotatably mounted with respect to missile housing
    • 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
FR938892A 1962-06-30 1963-06-21 Rocket projectile stabilized in rotation Expired FR1363559A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR938892A FR1363559A (en) 1962-06-30 1963-06-21 Rocket projectile stabilized in rotation

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DER33038A DE1213760B (en) 1962-06-30 1962-06-30 Self-propelled hollow charge projectile
FR938892A FR1363559A (en) 1962-06-30 1963-06-21 Rocket projectile stabilized in rotation

Publications (1)

Publication Number Publication Date
FR1363559A true FR1363559A (en) 1964-06-12

Family

ID=25991570

Family Applications (1)

Application Number Title Priority Date Filing Date
FR938892A Expired FR1363559A (en) 1962-06-30 1963-06-21 Rocket projectile stabilized in rotation

Country Status (1)

Country Link
FR (1) FR1363559A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITVR20130268A1 (en) * 2013-12-04 2015-06-05 M G R S R L JET ENGINE WITH CONFORMED RING NOZZLE FOR SEMIAUTOPROPULSA RIFLE BOMBS AS WELL AS BI-PLURI MISSILES AND STADIUM ROCKERS OF ARTILLERY OR PLURISTADIUM ARTILLERY PROJECTS WITH CORRECTION OF THE TRAJECTORY WITH ADDITIONAL PROJECT, RAZZ

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITVR20130268A1 (en) * 2013-12-04 2015-06-05 M G R S R L JET ENGINE WITH CONFORMED RING NOZZLE FOR SEMIAUTOPROPULSA RIFLE BOMBS AS WELL AS BI-PLURI MISSILES AND STADIUM ROCKERS OF ARTILLERY OR PLURISTADIUM ARTILLERY PROJECTS WITH CORRECTION OF THE TRAJECTORY WITH ADDITIONAL PROJECT, RAZZ

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