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Industry
CPC
F42B10/00
This industry / category may be too specific. Please go to a parent level for more data
Parent Industries
F
MECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS
F42
Ammunition
F42B
EXPLOSIVE CHARGES
Current Industry
F42B10/00
Means for influencing
Sub Industries
F42B10/02
Stabilising arrangements
F42B10/025
using giratory or oscillating masses for stabilising projectile trajectory
F42B10/04
using fixed fins
F42B10/06
Tail fins
F42B10/08
Flechette-type projectiles
F42B10/10
the fins being formed in the barrel by deformation or the projectile body
F42B10/12
using fins longitudinally-slidable with respect to the projectile or missile
F42B10/14
using fins spread or deployed after launch
F42B10/143
Lattice or grid fins
F42B10/146
Fabric fins
F42B10/16
Wrap-around fins
F42B10/18
using a longitudinally slidable support member
F42B10/20
deployed by combustion gas pressure, or by pneumatic or hydraulic forces
F42B10/22
Projectiles of cannelured type
F42B10/24
with inclined grooves
F42B10/26
using spin
F42B10/28
induced by gas action
F42B10/30
using rocket motor nozzles
F42B10/32
Range-reducing or range-increasing arrangements Fall-retarding means
F42B10/34
Tubular projectiles
F42B10/36
Ring-foil projectiles
F42B10/38
Range-increasing arrangements
F42B10/40
with combustion of a slow-burning charge
F42B10/42
Streamlined projectiles
F42B10/44
Boat-tails specially adapted for drag reduction
F42B10/46
Streamlined nose cones Windshields Radomes
F42B10/48
Range-reducing, destabilising or braking arrangements
F42B10/50
Brake flaps
F42B10/52
Nose cones
F42B10/54
Spin braking means
F42B10/56
of parachute or paraglider type
F42B10/58
of rotochute type
F42B10/60
Steering arrangements
F42B10/62
Steering by movement of flight surfaces
F42B10/64
of fins
F42B10/66
Steering by varying intensity or direction of thrust
F42B10/661
using several transversally acting rocket motors, each motor containing an individual propellant charge
F42B10/663
using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
F42B10/665
characterised by using a nozzle provided with at least a deflector mounted within the nozzle
F42B10/666
characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
F42B10/668
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