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.)
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.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AGfiledCriticalWerkzeugmaschinenfabrik Oerlikon Buhrle AG
Application grantedgrantedCritical
Publication of DE883862CpublicationCriticalpatent/DE883862C/de
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
F42B10/04—Stabilising arrangements using fixed fins
F42B10/06—Tail fins
Landscapes
Physics & Mathematics
(AREA)
Fluid Mechanics
(AREA)
Engineering & Computer Science
(AREA)
General Engineering & Computer Science
(AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets
(AREA)
New researches on small span-chord ratio wings with lateral jets(Lift increase of small span-chord ratio wings with lateral fluid jets directed along span)
An extension of Ackeret's theory for the study of infinite aspect ratio wings and rectangular or trapezoidal wings(Ackeret theory for infinite aspect ratio, rectangular and trapezoidal constant cord wings with arbitrary spanwise variation of profile in supersonic flow)
VTOL instrument flight research relating to aircraft requirements and operating characteristics for the terminal area(VTOL aircraft instrument flight in terminal area, defining requirements and operating characteristics for vertical and low speed capabilities)
The sequential spark technique- A tool for wake velocity studies in ballistic ranges(Sequential electric spark technique for hypervelocity projectiles turbulent wake velocity measurements at ballistic ranges in free flight regime)