GB1152198A - Missile Launch Simulator - Google Patents

Missile Launch Simulator

Info

Publication number
GB1152198A
GB1152198A GB37852/66A GB3785266A GB1152198A GB 1152198 A GB1152198 A GB 1152198A GB 37852/66 A GB37852/66 A GB 37852/66A GB 3785266 A GB3785266 A GB 3785266A GB 1152198 A GB1152198 A GB 1152198A
Authority
GB
United Kingdom
Prior art keywords
missile
launching
tube
simulator
dummy
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
GB37852/66A
Inventor
Maurice H Baller
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.)
US Department of Navy
Original Assignee
US Department of Navy
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 US Department of Navy filed Critical US Department of Navy
Publication of GB1152198A publication Critical patent/GB1152198A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A33/00—Adaptations for training; Gun simulators

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1,152,198. Missile launch simulator. UNITED STATES OF AMERICA, NAVY, SECRETARY OF. 23 Aug., 1966 [23 Aug., 1965], No. 37852/66. Heading F3C. A missile launch simulator comprises an underwater tube type missile launching system comprising a launching tube 21 within a supporting tube 22 in which the tactical moisture probe is replaced by a dummy moisture probe 44 and dynamic missile simulators 43 are arranged on the missile support ring 24. The missile control center 41 is provided with a dummy triggering inverter unit 42. The missile launching system further comprises a rupturable diaphragm 39 which covers the tube 21 and normally protects a missile from seawater when a hatch 30 of the system is opened. When used as a simulator the missile launching system tube 21 is filled with water 51 equivalent to the weight of an operational missile, the tube 21 being pressurized through a snorted unit 54. On the launching command being generated from the missile control center 41 a departure switch plunger is released by each dynamic simulator 43 to simulate the missiles first motion. The dummy triggering inverter unit 42 transmits a release signal from a launching relay to missile simulator solenoids of the dynamic simulators 43 upon launch command. The diaphragm 39 is then ruptured and the launching tube 21 fills with water to effect post launching conditions. The rupturing of the diaphragm 39 may be delayed by an electrical signal delay located in a box 55 for several simulated firings to give the "ripple" effect caused normally by multiple missile launchings.
GB37852/66A 1965-08-23 1966-08-23 Missile Launch Simulator Expired GB1152198A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US481990A US3386188A (en) 1965-08-23 1965-08-23 Missile launch simulator

Publications (1)

Publication Number Publication Date
GB1152198A true GB1152198A (en) 1969-05-14

Family

ID=23914201

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37852/66A Expired GB1152198A (en) 1965-08-23 1966-08-23 Missile Launch Simulator

Country Status (2)

Country Link
US (1) US3386188A (en)
GB (1) GB1152198A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2441825A1 (en) * 1978-11-16 1980-06-13 British Aerospace MISSILE LAUNCHING DEVICE

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102923281A (en) * 2012-04-05 2013-02-13 周松林 Submarine type missile launching platform
CN107702594B (en) * 2017-10-24 2023-07-04 北京云创太和科技有限公司 Missile decoy and missile vehicle
CN108413807B (en) * 2018-05-04 2023-10-03 山西华洋吉禄科技股份有限公司 Device for simulating missile to leave cabin rapidly

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3075301A (en) * 1961-07-13 1963-01-29 Willy A Fiedler Launch and underwater trajectory test vehicle
US3075302A (en) * 1961-08-17 1963-01-29 Willy A Fiedler Underwater pitch-over launch test vehicle
US3100421A (en) * 1962-01-08 1963-08-13 Tsoy K Moy Post-launch flooding control apparatus
US3128671A (en) * 1962-12-31 1964-04-14 William H Mairs Dynamic missile simulator
US3276150A (en) * 1965-03-15 1966-10-04 Hamilton Russell Disposable sabot

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2441825A1 (en) * 1978-11-16 1980-06-13 British Aerospace MISSILE LAUNCHING DEVICE

Also Published As

Publication number Publication date
US3386188A (en) 1968-06-04

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLE Entries relating assignments, transmissions, licences in the register of patents
PLNP Patent lapsed through nonpayment of renewal fees