RT01
|
The projectile shall contain a thermally actionable luminescent chemical marker |
RT02
|
The propulsion subsystem shall be disconnected from the projectile right after firing |
RT03
|
The additional propulsion charges cases shall be arranged longitudinally along the axis of the charge-carrying tube |
RT04
|
The additional propulsion charges cases shall be covered by impermeable nitrocellulose film |
RT05
|
The propellant charges must contain modified pyroxylin powder with low dependence on the combustion rate related to the pressure |
RT06
|
The initial propulsion charge shall be contained in cylindrical cartridge with a length to diameter ratio of 5.5 / 6.5 |
RT07
|
The initial propulsion cartridge shall be inserted in a metal tube with a perforation to surface ratio of 0.030 / 0.035 |
RT08
|
The initial propulsion cartridge shall contain a primer igniter with black powder at the rate of 5.0 / 5.5% by weight related to the initial propulsion load |
RT09
|
The projectile shall contain an additional propulsion charge inside the grenade with delayed trigger mechanism with an exclusive igniter |
RT10
|
The projectile shall contain articulated aerodynamic fins which open after firing fixed to the grenade by means of a rod |
RT11
|
The grenade shall contain a fuze in its lower part with a pyrotechnic device for delayed trigger mechanism composed by a transmission charge with low burning rate |
RT12
|
The grenade shall have protrusions on its inner surface which prevent the movement of the main explosive charge |
RT13
|
The grenade shall have a previously fragmented coating with lower tensile strength |
RT14
|
The fins shall be made of lightweight metal alloy |
RT15
|
The fins shall be coupled to an ejectable propulsion device containing grooves on its outer surface capable of preventing the exhaust of the propulsion gases during firing |
RT16
|
The fins shall comprise retractable stabilizing flaps holded by an ejection device containing grooves on its outer surface capable of preventing the escape of the propulsion gases during the firing |
RT17
|
The projectile shall have a diametrically opposite pair of side fins located at the rear of the shell body in addition to the stabilizing fins |
RT18
|
The projectile shall have the tip angle formed by the fuze and the shell body up to its maximum diameter between 4° and 20° |
RT19
|
The projectile shall contain a self-propelled charge with exclusive igniter with delayed trigger mechanism coupled to an ejectable propulsion device |
RT20
|
The stabilization fins shall have oblique radial edge and a parallel axial edge related to the longitudinal axis of the ammunition in order to deflect the air against the side face of the fins |
RT21
|
The grenade shall have a metal skirt at its rear that allows the ammunition to fall through the tube of the weapon and whose end can be expanded by the propulsion gases in order to retain them inside the tube during firing |
RT22
|
The fuze must contain a delaying mechanism adjustable by external key |
RT23
|
The stabilization fins shall have rectangular plates coupled transversely to their respective rear edges |
RT24
|
The initial propulsion cartridge shall consist of a tube containing the propellant charge with the top end closed and the bottom end connected to the base containing the igniter being both parts made of synthetic polymer |
RT25
|
The initial propulsion cartridge shall consist of a tube containing the propellant charge with the top end closed and the bottom end connected to the base containing the igniter through grooves and protrusions |
RT26
|
The initial propulsion cartridge shall be fixed within the fins axial tube by a deformable polymer flange |
RT27
|
The grenade shall have spherical steel projectiles stored inside the wall |
RT28
|
The fuze shall have a safety mechanism which allows the alignment of the explosive chain after firing through a retractable fin which opens due to the air resistance |
RT29
|
The main explosive charge shall be PETN |
RT30
|
The fuze shall have an explosive chain consisting of a sequence of explosives with a decreasing sensitivity up to the main charge with a density change of 1.2 to 1.7 g/cm 3
|
RT31
|
The fuze shall have deformable side sections linked to axial bores capable of conveying oblique impact |
RT32
|
The propulsion cartridge shall have an initial charge in the longitudinal axis of the ammunition and additional concentric charges parallel to the first axis and triggered by the initial charge through selective holes |
RT33
|
The initial propulsion cartridge shall have two igniters located at opposite ends connected by axial tube in order to trigger the projection charge located on the side of the cartridge in a downward direction |