FR2336654A1 - Dispositif de visee pour projectile ou engin autopropulse - Google Patents

Dispositif de visee pour projectile ou engin autopropulse

Info

Publication number
FR2336654A1
FR2336654A1 FR7539708A FR7539708A FR2336654A1 FR 2336654 A1 FR2336654 A1 FR 2336654A1 FR 7539708 A FR7539708 A FR 7539708A FR 7539708 A FR7539708 A FR 7539708A FR 2336654 A1 FR2336654 A1 FR 2336654A1
Authority
FR
France
Prior art keywords
disc
cylindrical wall
cut away
pitosphorescent
launching tube
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
FR7539708A
Other languages
English (en)
Other versions
FR2336654B1 (fr
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.)
Ruggieri SA
Original Assignee
Ruggieri 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 Ruggieri SA filed Critical Ruggieri SA
Priority to FR7539708A priority Critical patent/FR2336654A1/fr
Publication of FR2336654A1 publication Critical patent/FR2336654A1/fr
Application granted granted Critical
Publication of FR2336654B1 publication Critical patent/FR2336654B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G1/00Sighting devices
    • F41G1/44Spirit-level adjusting means, e.g. for correcting tilt; Means for indicating or correcting tilt or cant

Landscapes

  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Telescopes (AREA)
  • Toys (AREA)
FR7539708A 1975-12-24 1975-12-24 Dispositif de visee pour projectile ou engin autopropulse Granted FR2336654A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7539708A FR2336654A1 (fr) 1975-12-24 1975-12-24 Dispositif de visee pour projectile ou engin autopropulse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7539708A FR2336654A1 (fr) 1975-12-24 1975-12-24 Dispositif de visee pour projectile ou engin autopropulse

Publications (2)

Publication Number Publication Date
FR2336654A1 true FR2336654A1 (fr) 1977-07-22
FR2336654B1 FR2336654B1 (fr) 1982-08-20

Family

ID=9164157

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7539708A Granted FR2336654A1 (fr) 1975-12-24 1975-12-24 Dispositif de visee pour projectile ou engin autopropulse

Country Status (1)

Country Link
FR (1) FR2336654A1 (fr)

Also Published As

Publication number Publication date
FR2336654B1 (fr) 1982-08-20

Similar Documents

Publication Publication Date Title
ES450215A1 (es) Sistema de control de actitud de un cuerpo cilindrico en desplazamiento en un fluido e ingenio que incorpora dicho sistema.
ES2081904T3 (es) Sistema de guia para misiles de peso ligero.
FR2336654A1 (fr) Dispositif de visee pour projectile ou engin autopropulse
SE8902228D0 (sv) Vapenarrangemang
GB1422404A (en) Infantry protectile
GB1527971A (en) Finned tail unit for a missile
Hostetler et al. Sandia inertial terrain-aided navigation system
ES216821Y (es) Dispositivo de disparo para lanzar proyectiles de armas de caza submarina.
GB846236A (en) Sighting device for rifle grenades and the like
ATE153755T1 (de) Abschussvorrichtung für mörsergeschoss
FR2323981A1 (fr) Munition d'exercice
FR2296863A1 (fr) Nouveau capuchon de protection pour lunette de visee et organes analogues
STEWART A study of guidance schemes for air-to-air missiles(Evaluation of various guidance schemes for air to air homing missiles)[M. S. Thesis]
FR2371125A5 (fr) Bati de lancement pour engins volants dirigeables
BENSO et al. Effect of position and azimuth errors in a shipboard inertial navigation system on the radial miss of a sea launched missile
GB1207743A (en) Firing equipment and an adapter device therefor
NEUPOKOEV Self-guidance system of an antiaircraft guided missile
FR2331768A1 (fr) Grenade perfectionnee
GB987917A (en) Improvements in and relating to movable targets for shooting
AGGARWAL Light gas guns(hypervelocity launchers for ballistic range test tunnels)
Drucker The determination of tracking system require- ments and the design of an optimized test regime for evaluating ballistic missile inertial guidance systems in flight test(Tracking system requirements and design of optimized test regime for evaluating ballistic missile inertial guidance systems in flight test)
TOWER Two dimensional mathematical model of a propellant lined hypervelocity launch tube[Ph. D. Thesis]
Konrad et al. Techniques for determining velocity and position of small hypervelocity spheres
GB1321893A (en) Projectile for line projecting gun
JO915B1 (en) Gyro target finder device

Legal Events

Date Code Title Description
ST Notification of lapse