GB676368A - Improvements in or relating to rocket missiles - Google Patents

Improvements in or relating to rocket missiles

Info

Publication number
GB676368A
GB676368A GB13016/49A GB1301649A GB676368A GB 676368 A GB676368 A GB 676368A GB 13016/49 A GB13016/49 A GB 13016/49A GB 1301649 A GB1301649 A GB 1301649A GB 676368 A GB676368 A GB 676368A
Authority
GB
United Kingdom
Prior art keywords
ring
nozzle
rocket
relating
nordstrom
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
GB13016/49A
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.)
INGA TORA MARIA NORDSTROEM
SVEN HUGO NORDSTROEM
Original Assignee
INGA TORA MARIA NORDSTROEM
SVEN HUGO NORDSTROEM
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 INGA TORA MARIA NORDSTROEM, SVEN HUGO NORDSTROEM filed Critical INGA TORA MARIA NORDSTROEM
Publication of GB676368A publication Critical patent/GB676368A/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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

676,368. Rocket propulsion. BRODEN, E. W., NORDSTROM, S. H., and NORDSTROM, I. T. M. May 16, 1949. [May 18, 1948] No. 13016/49. Class 9 (ii). A rocket 1 has a combustion chamber 2 from which the gases produced on combustion of the propellant are exhausted through a Laval nozzle 3. Between the chamber 2 and the nozzle is placed a ring 4 provided with inclined vanes and within the ring is a streamlined body 5. Thus the ring 4 combined with the body 5 form a turbine wheel fixed in the projectile so that the gases are deflected and cause the projectile to rotate. In a modification the ring 4 and the body 5 are placed within the nozzle exit. The outer ends of the inclined vanes are attached to the inside wall of the nozzle or combustion chamber as by welding or by fixing in splines.
GB13016/49A 1948-05-18 1949-05-16 Improvements in or relating to rocket missiles Expired GB676368A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE676368X 1948-05-18

Publications (1)

Publication Number Publication Date
GB676368A true GB676368A (en) 1952-07-23

Family

ID=20314768

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13016/49A Expired GB676368A (en) 1948-05-18 1949-05-16 Improvements in or relating to rocket missiles

Country Status (1)

Country Link
GB (1) GB676368A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3066484A (en) * 1961-04-10 1962-12-04 Earl H Buchanan Gas flow control rocket motor device
US3712061A (en) * 1966-11-02 1973-01-23 Us Navy Vortex baffle
FR2848658A1 (en) * 1995-04-24 2004-06-18 United Kingdom Government LARGE RANGE ARTILLERY SHELL
US7360355B1 (en) * 1996-06-07 2008-04-22 Qinetiq Limited Long range artillery shell

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3066484A (en) * 1961-04-10 1962-12-04 Earl H Buchanan Gas flow control rocket motor device
US3712061A (en) * 1966-11-02 1973-01-23 Us Navy Vortex baffle
FR2848658A1 (en) * 1995-04-24 2004-06-18 United Kingdom Government LARGE RANGE ARTILLERY SHELL
DE19648668B4 (en) * 1995-04-24 2008-03-27 Qinetiq Ltd. Long-range artillery shell
US7360355B1 (en) * 1996-06-07 2008-04-22 Qinetiq Limited Long range artillery shell

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