FR2635180B1 - Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques - Google Patents

Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques

Info

Publication number
FR2635180B1
FR2635180B1 FR8810641A FR8810641A FR2635180B1 FR 2635180 B1 FR2635180 B1 FR 2635180B1 FR 8810641 A FR8810641 A FR 8810641A FR 8810641 A FR8810641 A FR 8810641A FR 2635180 B1 FR2635180 B1 FR 2635180B1
Authority
FR
France
Prior art keywords
control
propulsion assembly
ballistic objects
ballistic
objects
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
FR8810641A
Other languages
English (en)
Other versions
FR2635180A1 (fr
Inventor
Claudio Peretti
Guglielmo Rebuffatti
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.)
ARIS SpA
Original Assignee
ARIS SpA
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 ARIS SpA filed Critical ARIS SpA
Publication of FR2635180A1 publication Critical patent/FR2635180A1/fr
Application granted granted Critical
Publication of FR2635180B1 publication Critical patent/FR2635180B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
FR8810641A 1988-08-05 1988-08-05 Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques Expired - Lifetime FR2635180B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/228,973 US4892268A (en) 1988-08-05 1988-08-05 Propulsion, monitoring and control unit particularly for ballistic objects

Publications (2)

Publication Number Publication Date
FR2635180A1 FR2635180A1 (fr) 1990-02-09
FR2635180B1 true FR2635180B1 (fr) 1992-11-06

Family

ID=22859305

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8810641A Expired - Lifetime FR2635180B1 (fr) 1988-08-05 1988-08-05 Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques

Country Status (3)

Country Link
US (1) US4892268A (fr)
DE (1) DE3826702A1 (fr)
FR (1) FR2635180B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6276277B1 (en) 1999-04-22 2001-08-21 Lockheed Martin Corporation Rocket-boosted guided hard target penetrator
US6494140B1 (en) 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
DE102008014257B4 (de) * 2008-03-13 2009-12-03 Diehl Bgt Defence Gmbh & Co. Kg Lenkflugkörper
SE541615C2 (sv) * 2017-04-28 2019-11-12 Bae Systems Bofors Ab Projektil med valbar anfallsvinkel

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423090A (en) * 1943-08-25 1947-07-01 Fink Rudolph Controllable gliding attachment for bombs
US2926611A (en) * 1944-10-28 1960-03-01 Jr Wilbur S Hinman Circuit controlling means
FR2165695B1 (fr) * 1970-04-30 1976-02-06 Hawker Siddeley Dynamics Gb
DE3027841A1 (de) * 1980-07-23 1982-02-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "zufuehrung der treibstoffe vom flugkoerper zu einem an diesem winkelbeweglich aufgehaengten rueckstosstriebwerk, insbesondere raketentriebwerk"
DE3132190A1 (de) * 1981-08-14 1983-03-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Tragvorrichtung fuer eine abwurflast an einem flugzeug
US4553718A (en) * 1982-09-30 1985-11-19 The Boeing Company Naval harrassment missile

Also Published As

Publication number Publication date
DE3826702A1 (de) 1990-02-15
US4892268A (en) 1990-01-09
FR2635180A1 (fr) 1990-02-09

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Legal Events

Date Code Title Description
ST Notification of lapse