SE333317B - NON-ROTATION-CONTROLLED ROCKET DEVICE - Google Patents
NON-ROTATION-CONTROLLED ROCKET DEVICEInfo
- Publication number
- SE333317B SE333317B SE9747/67A SE974767A SE333317B SE 333317 B SE333317 B SE 333317B SE 9747/67 A SE9747/67 A SE 9747/67A SE 974767 A SE974767 A SE 974767A SE 333317 B SE333317 B SE 333317B
- Authority
- SE
- Sweden
- Prior art keywords
- rotation
- rocket device
- controlled rocket
- controlled
- rocket
- Prior art date
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
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- 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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US570124A US3319566A (en) | 1966-07-25 | 1966-07-25 | Non-spin rockets and their guidance |
Publications (1)
Publication Number | Publication Date |
---|---|
SE333317B true SE333317B (en) | 1971-03-08 |
Family
ID=24278342
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE9747/67A SE333317B (en) | 1966-07-25 | 1967-06-29 | NON-ROTATION-CONTROLLED ROCKET DEVICE |
Country Status (4)
Country | Link |
---|---|
US (1) | US3319566A (en) |
BE (1) | BE701786A (en) |
NO (1) | NO122905B (en) |
SE (1) | SE333317B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3390850A (en) * | 1967-08-04 | 1968-07-02 | Army Usa | Fin for inducing spin in rotating rockets |
US4046076A (en) * | 1975-09-29 | 1977-09-06 | The United States Of America As Represented By The Secretary Of The Navy | Impulsive rocket motor safety-arming device |
US5596166A (en) * | 1994-12-28 | 1997-01-21 | Logicon Rda | Penetrating vehicle with rocket motor |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2503271A (en) * | 1945-02-06 | 1950-04-11 | Clarence N Hickman | Rocket projectile |
US2946261A (en) * | 1956-05-02 | 1960-07-26 | Sydney R Crockett | Peripheral nozzle spinner rocket |
US3176615A (en) * | 1962-12-31 | 1965-04-06 | Avco Corp | Gun-propelled rocket-boosted missile |
-
1966
- 1966-07-25 US US570124A patent/US3319566A/en not_active Expired - Lifetime
-
1967
- 1967-05-18 NO NO168189A patent/NO122905B/no unknown
- 1967-06-29 SE SE9747/67A patent/SE333317B/en unknown
- 1967-07-25 BE BE701786D patent/BE701786A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
US3319566A (en) | 1967-05-16 |
BE701786A (en) | 1968-01-25 |
NO122905B (en) | 1971-08-30 |
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