JPS53128200A - Antivibration method of instrument in guided missile - Google Patents

Antivibration method of instrument in guided missile

Info

Publication number
JPS53128200A
JPS53128200A JP4233577A JP4233577A JPS53128200A JP S53128200 A JPS53128200 A JP S53128200A JP 4233577 A JP4233577 A JP 4233577A JP 4233577 A JP4233577 A JP 4233577A JP S53128200 A JPS53128200 A JP S53128200A
Authority
JP
Japan
Prior art keywords
instrument
guided missile
antivibration
antivibration method
launching
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.)
Pending
Application number
JP4233577A
Other languages
Japanese (ja)
Inventor
Hisashi Iga
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP4233577A priority Critical patent/JPS53128200A/en
Publication of JPS53128200A publication Critical patent/JPS53128200A/en
Pending 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
    • F42B15/08—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles for carrying measuring instruments; Arrangements for mounting sensitive cargo within a projectile; Arrangements for acoustic sensitive cargo within a projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Dampers (AREA)

Abstract

PURPOSE:To obtain suitable antivibration effect to instruments in guided missile, by fixing instrument with frame before launching and by connecting the instrument through antivibration members with the frame after launching to adopt for vibration acceleration on the instrument.
JP4233577A 1977-04-13 1977-04-13 Antivibration method of instrument in guided missile Pending JPS53128200A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4233577A JPS53128200A (en) 1977-04-13 1977-04-13 Antivibration method of instrument in guided missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4233577A JPS53128200A (en) 1977-04-13 1977-04-13 Antivibration method of instrument in guided missile

Publications (1)

Publication Number Publication Date
JPS53128200A true JPS53128200A (en) 1978-11-08

Family

ID=12633129

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4233577A Pending JPS53128200A (en) 1977-04-13 1977-04-13 Antivibration method of instrument in guided missile

Country Status (1)

Country Link
JP (1) JPS53128200A (en)

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