SE362951B - - Google Patents

Info

Publication number
SE362951B
SE362951B SE08915/71A SE891571A SE362951B SE 362951 B SE362951 B SE 362951B SE 08915/71 A SE08915/71 A SE 08915/71A SE 891571 A SE891571 A SE 891571A SE 362951 B SE362951 B SE 362951B
Authority
SE
Sweden
Application number
SE08915/71A
Inventor
F A Donner
T Kronholm
Original Assignee
Tampella Oy Ab
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 Tampella Oy Ab filed Critical Tampella Oy Ab
Publication of SE362951B publication Critical patent/SE362951B/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/04Stabilising arrangements using fixed fins
    • F42B10/06Tail fins
SE08915/71A 1970-07-11 1971-07-09 SE362951B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2034569A DE2034569C3 (en) 1970-07-11 1970-07-11 Tail unit for wing-stabilized projectiles

Publications (1)

Publication Number Publication Date
SE362951B true SE362951B (en) 1973-12-27

Family

ID=5776549

Family Applications (1)

Application Number Title Priority Date Filing Date
SE08915/71A SE362951B (en) 1970-07-11 1971-07-09

Country Status (10)

Country Link
US (1) US3756539A (en)
CA (1) CA948030A (en)
DE (1) DE2034569C3 (en)
DK (1) DK131586C (en)
FI (1) FI53500C (en)
FR (1) FR2099881A5 (en)
GB (1) GB1300361A (en)
IL (1) IL37028A (en)
NO (1) NO129818B (en)
SE (1) SE362951B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES8706942A1 (en) * 1986-04-16 1987-07-01 Esperanza & Cie Sa Mortar grenade
DE3927918A1 (en) * 1989-08-24 1991-02-28 Rheinmetall Gmbh Armour piercing projectile guiding fins - lie close to projectile body so that fin tip is inside boundary layer
US5158509A (en) * 1990-12-14 1992-10-27 The United States Of America As Represented By The United States Department Of Energy Composite stabilizer unit
SE517003C2 (en) * 2000-09-05 2002-04-02 Bofors Defence Ab Ways to increase the firing range of finely equipped artillery projectiles and such projectiles
DE102009035967A1 (en) * 2009-08-04 2011-02-10 Rheinmetall Waffe Munition Gmbh Mortar shell, has tail shaft connected with projectile body, and wing tail unit tail-laterally fastened in tail shaft, which comprises material with high tensile strength than material of wing tail unit
US20220373308A1 (en) * 2021-05-12 2022-11-24 Crossbullet, Llc Projectile and firearm system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE379532A (en) * 1930-05-22
GB431551A (en) * 1933-12-01 1935-07-10 Jean Fabry Improvements in stabilising and damping devices
FR802042A (en) * 1935-05-12 1936-08-25 Self-correcting stabilizer
US2597703A (en) * 1946-02-07 1952-05-20 Us Navy Rocket fin

Also Published As

Publication number Publication date
DE2034569C3 (en) 1975-04-10
NO129818B (en) 1974-05-27
FR2099881A5 (en) 1972-03-17
FI53500B (en) 1978-01-31
CA948030A (en) 1974-05-28
DK131586B (en) 1975-08-04
GB1300361A (en) 1972-12-20
IL37028A (en) 1974-10-22
DE2034569A1 (en) 1972-01-13
US3756539A (en) 1973-09-04
IL37028A0 (en) 1971-11-29
FI53500C (en) 1978-05-10
DK131586C (en) 1976-01-05
DE2034569B2 (en) 1974-08-15

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