GB1307885A - Safe-starting control system for a missile - Google Patents
Safe-starting control system for a missileInfo
- Publication number
- GB1307885A GB1307885A GB2232670A GB2232670A GB1307885A GB 1307885 A GB1307885 A GB 1307885A GB 2232670 A GB2232670 A GB 2232670A GB 2232670 A GB2232670 A GB 2232670A GB 1307885 A GB1307885 A GB 1307885A
- Authority
- GB
- United Kingdom
- Prior art keywords
- control
- missile
- signal
- starting
- operative
- 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
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
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/40—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Direct Current Feeding And Distribution (AREA)
- Air Bags (AREA)
Abstract
1307885 Launching missiles RAFAUT & CIE 8 May 1970 [13 May 1969] 22326/70 Heading F3C The invention relates to a safe starting control system for a missile which is to be carried on and fired from a carrier vehicle, the system being adapted to control the starting of at least one control mechanism in the missile a predetermined time after it has been fired from the vehicle. The system comprises an electric cable 2 one end of which is adapted to be detachably connected to an electric power source provided on the carrier vehicle (not shown) and operative to supply an electric signal upon firing of the missile therefrom, a pyrotechnic time delay relay 5 electrically connected to the other end of the electric cable and operative to be ignited by the electric signal and to provide a mechanical signal after a predetermined time delay corresponding to the combustion period of the pyrotechnic relay, a transducer adapted to provide an electrical control signal in response to the mechanical signal and a starting mechanism 7 responsive to the electrical control signal from the transducer to control the start of the control mechanism or one or each of the control mechanisms. A switch 48 is provided which is operative to switch off the electrical connection between the time delay relay and the electric cable until the missile is detached from the carrier vehicle. A safety circuit 60 is provided so that a control signal accidentally produced by the transducer as a result of its receiving a shock will not operate the starting mechanism.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6915443A FR2041722A1 (en) | 1969-05-13 | 1969-05-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1307885A true GB1307885A (en) | 1973-02-21 |
Family
ID=9033965
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2232670A Expired GB1307885A (en) | 1969-05-13 | 1970-05-08 | Safe-starting control system for a missile |
Country Status (7)
Country | Link |
---|---|
US (1) | US3670654A (en) |
BE (1) | BE750274A (en) |
CH (1) | CH518213A (en) |
DE (1) | DE2023224A1 (en) |
ES (1) | ES379572A1 (en) |
FR (1) | FR2041722A1 (en) |
GB (1) | GB1307885A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3771412A (en) * | 1972-04-18 | 1973-11-13 | Us Air Force | Missile launcher |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR924687A (en) * | 1945-02-15 | 1947-08-12 | Automatic release device for parachutes | |
US2812148A (en) * | 1949-09-07 | 1957-11-05 | Gordon L Fogal | Delayed opening parachute pack |
US2826120A (en) * | 1952-07-29 | 1958-03-11 | Chance Vought Aircraft Inc | Mechanism for ejecting rockets from an aircraft |
US2845024A (en) * | 1953-01-08 | 1958-07-29 | Jr Robert E Greene | Safety arming device |
US2786393A (en) * | 1954-09-30 | 1957-03-26 | David D Grimes | Monitoring cable release mechanism |
US2775745A (en) * | 1955-06-22 | 1956-12-25 | Frederic N Eaton | Breakaway electrical connector |
US2918845A (en) * | 1957-11-08 | 1959-12-29 | Microloc Corp | Electric arming device |
CH358694A (en) * | 1958-03-12 | 1961-11-30 | Contraves Ag | Electrically steerable explosive projectile |
US3034471A (en) * | 1959-08-25 | 1962-05-15 | Vare Ind | Method of nesting an underwater towed vehicle |
US3518613A (en) * | 1968-03-27 | 1970-06-30 | Us Navy | Missile umbilical cable |
-
1969
- 1969-05-13 FR FR6915443A patent/FR2041722A1/fr active Pending
-
1970
- 1970-05-08 GB GB2232670A patent/GB1307885A/en not_active Expired
- 1970-05-11 US US36239A patent/US3670654A/en not_active Expired - Lifetime
- 1970-05-11 CH CH696870A patent/CH518213A/en not_active IP Right Cessation
- 1970-05-12 DE DE19702023224 patent/DE2023224A1/en active Pending
- 1970-05-12 ES ES379572A patent/ES379572A1/en not_active Expired
- 1970-05-12 BE BE750274D patent/BE750274A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE2023224A1 (en) | 1970-11-26 |
FR2041722A1 (en) | 1971-02-05 |
CH518213A (en) | 1972-01-31 |
US3670654A (en) | 1972-06-20 |
ES379572A1 (en) | 1972-10-16 |
BE750274A (en) | 1970-10-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1453106A (en) | Piezoelectric fuses | |
EP0301848A3 (en) | Blasting system and components therefor | |
SE9202119D0 (en) | DIGITAL DELAY DETONATOR | |
GB1021249A (en) | A relay for rocket weapons | |
US2545474A (en) | Delayed detonating means for projectiles | |
GB1262165A (en) | Hollow explosive charge missile | |
GB1360305A (en) | Tripping device for firing at least one electric primer by means of a remotely located pyrotechnic composition | |
GB1534134A (en) | Lure launching cartridges | |
US4155285A (en) | Mortars for firing smoke candles and explosive shells | |
GB1307885A (en) | Safe-starting control system for a missile | |
US3930449A (en) | Time delay initiator | |
GB866698A (en) | Improvements in or relating to electrical remote control systems for missiles | |
US3039363A (en) | Rocket firing relay | |
FR2385075A1 (en) | Charge scattering rocket propulsion system - has igniter charge to actuate excess of propulsive charge to destroy remaining parts | |
US3041937A (en) | Rocket control system | |
GB927055A (en) | Improvements in projectiles fitted with an electric generator of the inertia type | |
US2988991A (en) | Self destructive torpedo | |
ES265133A1 (en) | Projectiles fitted with and electric detonator operated by a generator of the inertia type | |
GB1450968A (en) | Proximity fuse | |
GB1320158A (en) | Spring urged pyrotechnically actuated control elements | |
GB1520101A (en) | Electrical fuse for projectiles and a short circuit therefor | |
GB938739A (en) | Improvements in systems comprising a cluster of rockets carried by a launching machine | |
FR2408112A1 (en) | Projective fuse with multiple safety devices - includes DC arming motor with electronic circuit controlled by inertia and pressure switches | |
GB1356555A (en) | Safety device on an explosive projectile | |
FR1605546A (en) | Sea-air missile firing mechanism - has electric detonator with time delay and mechanical safety device comprising retractable flap |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |