GB141187A - Improvements in and connected with rockets - Google Patents

Improvements in and connected with rockets

Info

Publication number
GB141187A
GB141187A GB856719A GB856719A GB141187A GB 141187 A GB141187 A GB 141187A GB 856719 A GB856719 A GB 856719A GB 856719 A GB856719 A GB 856719A GB 141187 A GB141187 A GB 141187A
Authority
GB
United Kingdom
Prior art keywords
rockets
line
torpedoes
rocket
senior
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
GB856719A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB856719A priority Critical patent/GB141187A/en
Publication of GB141187A publication Critical patent/GB141187A/en
Expired 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
    • 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
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles

Abstract

141,187. Senior, G. April 4, 1919. Line-throwing apparatus. - A rocket is described provided with an eye f on the base plug d for the attachment of a line. Specification 139,856, [Class 9 (ii), Torpedoes &c.], is referred to.
GB856719A 1919-04-04 1919-04-04 Improvements in and connected with rockets Expired GB141187A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB856719A GB141187A (en) 1919-04-04 1919-04-04 Improvements in and connected with rockets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB856719A GB141187A (en) 1919-04-04 1919-04-04 Improvements in and connected with rockets

Publications (1)

Publication Number Publication Date
GB141187A true GB141187A (en) 1920-04-15

Family

ID=9854946

Family Applications (1)

Application Number Title Priority Date Filing Date
GB856719A Expired GB141187A (en) 1919-04-04 1919-04-04 Improvements in and connected with rockets

Country Status (1)

Country Link
GB (1) GB141187A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2442528A (en) * 1943-11-20 1948-06-01 Aerial Products Inc Rocket device
US2606495A (en) * 1947-09-30 1952-08-12 Kilgore Inc Pyrotechnic device
US2944389A (en) * 1944-11-20 1960-07-12 Clarence E Weinland Rotating rocket motor and method of making same
US3419230A (en) * 1966-04-14 1968-12-31 Mb Assoc Nozzle
FR2380529A1 (en) * 1977-02-14 1978-09-08 Serat Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2442528A (en) * 1943-11-20 1948-06-01 Aerial Products Inc Rocket device
US2944389A (en) * 1944-11-20 1960-07-12 Clarence E Weinland Rotating rocket motor and method of making same
US2606495A (en) * 1947-09-30 1952-08-12 Kilgore Inc Pyrotechnic device
US3419230A (en) * 1966-04-14 1968-12-31 Mb Assoc Nozzle
FR2380529A1 (en) * 1977-02-14 1978-09-08 Serat Propulsive charge for projectiles, missiles or rockets - incorporating longitudinal inclined elements giving rotation, minimising weight, complexity and cost

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