FR2455802A1 - Missile with nose aerial deployed on projection - with attach distance twice that when aerial is retracted - Google Patents

Missile with nose aerial deployed on projection - with attach distance twice that when aerial is retracted

Info

Publication number
FR2455802A1
FR2455802A1 FR7909696A FR7909696A FR2455802A1 FR 2455802 A1 FR2455802 A1 FR 2455802A1 FR 7909696 A FR7909696 A FR 7909696A FR 7909696 A FR7909696 A FR 7909696A FR 2455802 A1 FR2455802 A1 FR 2455802A1
Authority
FR
France
Prior art keywords
aerial
nose
missile
tube
pins
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.)
Granted
Application number
FR7909696A
Other languages
French (fr)
Other versions
FR2455802B1 (en
Inventor
Michel Precoul
Marcel Moury
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.)
SERAT
Original Assignee
SERAT
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 SERAT filed Critical SERAT
Priority to FR7909696A priority Critical patent/FR2455802B1/en
Publication of FR2455802A1 publication Critical patent/FR2455802A1/en
Application granted granted Critical
Publication of FR2455802B1 publication Critical patent/FR2455802B1/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
    • F42C19/06—Electric contact parts specially adapted for use with electric fuzes
    • F42C19/07—Nose-contacts for projectiles or missiles
    • 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
    • F42B12/105—Protruding target distance or stand-off members therefor, e.g. slidably mounted
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/14—Impact fuzes, i.e. fuzes actuated only by ammunition impact operating at a predetermined distance from ground or target by means of a protruding member

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)

Abstract

The missile has a nose aerial extendable when the missile is fired, and comprises a body (1) and rear inner casing (2) containing explosive (3). The aerial comprises a hollow tube (8) guided in a ribbed plastics nose piece (5) surrounded by a semi-elastic foam nose (6) inside a sealing nose casing (12), a metallised outer surface of the nose piece and inner contact points (7) of the nose casing forming poles of an electrical firing circuit. The aerial tube (8) is retained retracted by pins (16) which engage in corresponding tube holes, the pins being located in the nose piece and biassed out of the holes by coil springs (17) but retained by the wall of a guide tube for the missile. Once fired from the tube, the pins release the aerial which is extended by a coaxial spring (13) and locked in its extended position by further pins.
FR7909696A 1979-04-18 1979-04-18 DEPLOYABLE ANTENNA FOR PROJECTILE, MISSILE OR MACHINE HEAD Expired FR2455802B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7909696A FR2455802B1 (en) 1979-04-18 1979-04-18 DEPLOYABLE ANTENNA FOR PROJECTILE, MISSILE OR MACHINE HEAD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7909696A FR2455802B1 (en) 1979-04-18 1979-04-18 DEPLOYABLE ANTENNA FOR PROJECTILE, MISSILE OR MACHINE HEAD

Publications (2)

Publication Number Publication Date
FR2455802A1 true FR2455802A1 (en) 1980-11-28
FR2455802B1 FR2455802B1 (en) 1985-11-22

Family

ID=9224404

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7909696A Expired FR2455802B1 (en) 1979-04-18 1979-04-18 DEPLOYABLE ANTENNA FOR PROJECTILE, MISSILE OR MACHINE HEAD

Country Status (1)

Country Link
FR (1) FR2455802B1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528764A1 (en) * 1982-06-18 1983-12-23 Lincrusta Munition shell with nose cone insulation cover - carrying impact detonation spokes pref. having casing core of expanded polyethylene
FR2539505A1 (en) * 1983-01-14 1984-07-20 Luchaire Sa Improved nose for a projectile
FR2549950A1 (en) * 1983-07-26 1985-02-01 Diehl Gmbh & Co SECONDARY AMMUNITION BODY WITH TARGET DETECTION DEVICE
DE3538093A1 (en) * 1984-10-30 1986-05-15 Société d'Etudes, de Réalisations et d'Applications Techniques (S.E.R.A.T.), Paris OPTO-ELECTRONIC IMPACT SENSOR FOR missiles, rockets and the like projectiles
US4770100A (en) * 1986-07-18 1988-09-13 Rheinmetall Gmbh Hollow charge subsidiary projectile including a projectile body and a fuze spacer at the front
US4944226A (en) * 1988-08-19 1990-07-31 General Dynamics Corp., Pomona Div. Expandable telescoped missile airframe
US5621185A (en) * 1986-10-02 1997-04-15 Spengler; Hans Warhead

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH198437A (en) * 1937-01-04 1938-06-30 Sageb Societe Anonyme De Gesti Projectile fitted with a rocket.
FR1137831A (en) * 1961-09-27 1957-06-04 Soc Tech De Rech Ind Improvements in electric projectile initiation
FR2070389A5 (en) * 1969-12-03 1971-09-10 Serat
FR2157152A5 (en) * 1971-10-20 1973-06-01 Serat Nose cone contactor for projectiles - with high degree of sensitivity
US3742854A (en) * 1965-05-26 1973-07-03 Us Navy Fuze
US3804020A (en) * 1973-04-17 1974-04-16 Avco Corp Safing and arming system for a projectile fuze and fluidic control means for use therewith
FR2287671A1 (en) * 1974-10-08 1976-05-07 Serat Anti-personnel missile with multiple gas compartments - has compartment receiving firing gas before passing to next compartment

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH198437A (en) * 1937-01-04 1938-06-30 Sageb Societe Anonyme De Gesti Projectile fitted with a rocket.
FR1137831A (en) * 1961-09-27 1957-06-04 Soc Tech De Rech Ind Improvements in electric projectile initiation
US3742854A (en) * 1965-05-26 1973-07-03 Us Navy Fuze
FR2070389A5 (en) * 1969-12-03 1971-09-10 Serat
FR2157152A5 (en) * 1971-10-20 1973-06-01 Serat Nose cone contactor for projectiles - with high degree of sensitivity
US3804020A (en) * 1973-04-17 1974-04-16 Avco Corp Safing and arming system for a projectile fuze and fluidic control means for use therewith
FR2287671A1 (en) * 1974-10-08 1976-05-07 Serat Anti-personnel missile with multiple gas compartments - has compartment receiving firing gas before passing to next compartment

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528764A1 (en) * 1982-06-18 1983-12-23 Lincrusta Munition shell with nose cone insulation cover - carrying impact detonation spokes pref. having casing core of expanded polyethylene
FR2539505A1 (en) * 1983-01-14 1984-07-20 Luchaire Sa Improved nose for a projectile
FR2549950A1 (en) * 1983-07-26 1985-02-01 Diehl Gmbh & Co SECONDARY AMMUNITION BODY WITH TARGET DETECTION DEVICE
DE3538093A1 (en) * 1984-10-30 1986-05-15 Société d'Etudes, de Réalisations et d'Applications Techniques (S.E.R.A.T.), Paris OPTO-ELECTRONIC IMPACT SENSOR FOR missiles, rockets and the like projectiles
US4770100A (en) * 1986-07-18 1988-09-13 Rheinmetall Gmbh Hollow charge subsidiary projectile including a projectile body and a fuze spacer at the front
US5621185A (en) * 1986-10-02 1997-04-15 Spengler; Hans Warhead
US4944226A (en) * 1988-08-19 1990-07-31 General Dynamics Corp., Pomona Div. Expandable telescoped missile airframe

Also Published As

Publication number Publication date
FR2455802B1 (en) 1985-11-22

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