IT1149076B - Struttura di involucro di ala per ali rientrabili ad auto-erezione, in particolare di missili - Google Patents

Struttura di involucro di ala per ali rientrabili ad auto-erezione, in particolare di missili

Info

Publication number
IT1149076B
IT1149076B IT49119/82A IT4911982A IT1149076B IT 1149076 B IT1149076 B IT 1149076B IT 49119/82 A IT49119/82 A IT 49119/82A IT 4911982 A IT4911982 A IT 4911982A IT 1149076 B IT1149076 B IT 1149076B
Authority
IT
Italy
Prior art keywords
enterable
missiles
erection
wings
self
Prior art date
Application number
IT49119/82A
Other languages
English (en)
Other versions
IT8249119A0 (it
Inventor
Tommaso Anthony Di
Ronald T Inglis
Richard C Worley
Original Assignee
Gen Dynamics Pomona Div
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 Gen Dynamics Pomona Div filed Critical Gen Dynamics Pomona Div
Publication of IT8249119A0 publication Critical patent/IT8249119A0/it
Application granted granted Critical
Publication of IT1149076B publication Critical patent/IT1149076B/it

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
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • E05C9/02—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with one sliding bar for fastening when moved in one direction and unfastening when moved in opposite direction; with two sliding bars moved in the same direction when fastening or unfastening
IT49119/82A 1982-02-10 1982-09-15 Struttura di involucro di ala per ali rientrabili ad auto-erezione, in particolare di missili IT1149076B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US34766082A 1982-02-10 1982-02-10

Publications (2)

Publication Number Publication Date
IT8249119A0 IT8249119A0 (it) 1982-09-15
IT1149076B true IT1149076B (it) 1986-12-03

Family

ID=23364680

Family Applications (1)

Application Number Title Priority Date Filing Date
IT49119/82A IT1149076B (it) 1982-02-10 1982-09-15 Struttura di involucro di ala per ali rientrabili ad auto-erezione, in particolare di missili

Country Status (17)

Country Link
JP (1) JPS58138998A (it)
KR (1) KR860000220B1 (it)
AU (1) AU530408B2 (it)
BE (1) BE894382A (it)
CA (1) CA1190434A (it)
CH (1) CH661347A5 (it)
DE (1) DE3234269C2 (it)
DK (1) DK153183C (it)
ES (1) ES8308060A1 (it)
FR (1) FR2521281B1 (it)
GB (1) GB2115117B (it)
HK (1) HK36588A (it)
IL (1) IL66624A (it)
IT (1) IT1149076B (it)
NL (1) NL184340C (it)
NO (1) NO150820C (it)
SE (1) SE452364B (it)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3403573A1 (de) * 1983-11-09 1985-08-08 Diehl GmbH & Co, 8500 Nürnberg Geschoss mit herausklappbaren fluegeln
GB8815060D0 (en) * 1988-06-24 1988-11-16 British Aerospace Fin assembly for projectile
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
DE4105142A1 (de) * 1991-02-20 1992-08-27 Diehl Gmbh & Co Projektil mit ausklappbarem leitwerk
FR2721702B1 (fr) * 1994-06-28 1996-08-14 Luchaire Defense Sa Dispositif de déploiement d'une ailette de projectile.
DE102004007311A1 (de) 2004-02-14 2005-09-01 Diehl Bgt Defence Gmbh & Co. Kg Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1715558A (en) * 1929-06-04 X t trunk lock
FR1490554A (fr) * 1966-05-03 1967-08-04 Ruggieri Ets Perfectionnement aux empennages déployants de roquettes
US3853288A (en) * 1967-07-17 1974-12-10 H Bode Encasement for the tail section of a rocket with a central nozzle and extendible control vanes
BE756110A (fr) * 1970-09-14 1971-02-15 Gohlke Werner Dispositif pour l'influence thermique des fonctions d'engins volants.
DE2623562A1 (de) * 1976-05-26 1977-12-08 Basf Ag Verfahren zur herstellung von glykolestern und deren folgeprodukten
US4351499A (en) * 1979-09-24 1982-09-28 General Dynamics Double fabric, retractable, self-erecting wing for missle

Also Published As

Publication number Publication date
BE894382A (fr) 1983-03-14
SE452364B (sv) 1987-11-23
ES515721A0 (es) 1983-08-16
FR2521281A1 (fr) 1983-08-12
IT8249119A0 (it) 1982-09-15
ES8308060A1 (es) 1983-08-16
DK410182A (da) 1983-08-11
NO150820B (no) 1984-09-10
NO150820C (no) 1985-01-09
JPS6364720B2 (it) 1988-12-13
FR2521281B1 (fr) 1986-06-06
NL184340C (nl) 1989-06-16
CH661347A5 (de) 1987-07-15
DK153183C (da) 1988-11-14
DK153183B (da) 1988-06-20
GB2115117A (en) 1983-09-01
IL66624A (en) 1986-04-29
AU530408B2 (en) 1983-07-14
SE8205200D0 (sv) 1982-09-13
JPS58138998A (ja) 1983-08-18
NL184340B (nl) 1989-01-16
DE3234269C2 (de) 1985-05-09
CA1190434A (en) 1985-07-16
NL8203531A (nl) 1983-09-01
NO823115L (no) 1983-08-11
KR840001706A (ko) 1984-05-16
SE8205200L (sv) 1983-08-11
DE3234269A1 (de) 1983-08-25
HK36588A (en) 1988-05-27
GB2115117B (en) 1985-11-06
KR860000220B1 (ko) 1986-03-15

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