DE262445C - - Google Patents
Info
- Publication number
- DE262445C DE262445C DENDAT262445D DE262445DA DE262445C DE 262445 C DE262445 C DE 262445C DE NDAT262445 D DENDAT262445 D DE NDAT262445D DE 262445D A DE262445D A DE 262445DA DE 262445 C DE262445 C DE 262445C
- Authority
- DE
- Germany
- Prior art keywords
- projectile
- wings
- control
- pendulum
- control surfaces
- 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.)
- Active
Links
- 238000005339 levitation Methods 0.000 claims description 6
- 239000000725 suspension Substances 0.000 claims 1
- 239000007789 gas Substances 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 3
- 210000000078 claw Anatomy 0.000 description 3
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 238000004880 explosion Methods 0.000 description 2
- 230000002028 premature Effects 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE262445C true DE262445C (cs) |
Family
ID=519907
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DENDAT262445D Active DE262445C (cs) |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE262445C (cs) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2935942A (en) * | 1946-07-29 | 1960-05-10 | Young John A De | Homing device |
| US2961928A (en) * | 1958-11-03 | 1960-11-29 | Rosenthal Henry | Folding wing projectile |
| US2968996A (en) * | 1959-07-13 | 1961-01-24 | Raymond I Strickland | Fin-stabilized, center-rotated rocket |
| US4228737A (en) * | 1954-10-27 | 1980-10-21 | Aai Corporation | Glide bomb |
-
0
- DE DENDAT262445D patent/DE262445C/de active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2935942A (en) * | 1946-07-29 | 1960-05-10 | Young John A De | Homing device |
| US4228737A (en) * | 1954-10-27 | 1980-10-21 | Aai Corporation | Glide bomb |
| US2961928A (en) * | 1958-11-03 | 1960-11-29 | Rosenthal Henry | Folding wing projectile |
| US2968996A (en) * | 1959-07-13 | 1961-01-24 | Raymond I Strickland | Fin-stabilized, center-rotated rocket |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE3609092A1 (de) | Geschoss fuer eine rohrwaffe zum bekaempfen aktiv und passiv reagierender sonderpanzerungen | |
| DE2924450C2 (cs) | ||
| DE262445C (cs) | ||
| DE637594C (de) | Tragbare Feuerwaffe mit zum Werfen von Bomben dienendem Wurfrohr | |
| DE1942426A1 (de) | Fahrzeugaufhaengungen | |
| DE3603623C2 (cs) | ||
| DE694533C (de) | Einrichtung zur Steuerung von Raketen, insbesondere Raketengeschossen | |
| DE1578136B2 (de) | Geschoss mit stabilisierungsflossen | |
| DE3523443C1 (de) | Abdeckhaube fuer Munitions- und Abschussbehaelter von Flugzeugen | |
| DE713312C (de) | Reaktionsfrei arbeitender Impulsverstaerker | |
| DE3503041C1 (de) | Schnellfliegender Flugkörper mit aerodynamischer Steuerung | |
| EP0255570A1 (de) | Treibspiegelgeschoss, insbesondere Pfeilgeschoss | |
| DE2222785A1 (de) | Infanteriegeschoss zur bekaempfung von erdzielen | |
| DE2405128B2 (de) | Volumenregler mit einem druckdifferenzgesteuerten Membranelement | |
| DE2856286C2 (de) | Mit Überschallgeschwindigkeit fliegendes Geschoß | |
| DE1944152C3 (de) | Munition, bestehend aus einem Abschußrohr und einem darin befindlichen Flugkörper | |
| DE1925055A1 (de) | Flugkoerper mit einschwenkbaren Leitflaechen | |
| DE102006019758A1 (de) | Aufklärungseinrichtung | |
| DE935710C (de) | Lehrmunition schweren Kalibers | |
| DE130755C (cs) | ||
| DE69813381T2 (de) | Verfahren zum Kontrollieren der seitlichen Streuung von kreiselstabilisierten Geschossen | |
| AT201476B (de) | Durch Rückstoß angetriebener Körper | |
| EP1106958A1 (de) | Flugkörper | |
| DE1149639B (de) | Geschoss oder Flugkoerper mit Vortriebsladung | |
| DE3437307C1 (de) | Munition |