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PCE
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CPC Main Group
F41A 1/00

Missile propulsion characterised by the use of explosive or combustible propellant charges (projecting missiles without use of explosive or combustible propellant charge F41B; launching rockets or torpedoes F41F3/00; missile self-propulsion F42B15/00)

4 direct subcodes

Child Classifications

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  • F41A 1/02 Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion
  • F41A 1/04 Missile propulsion using the combustion of a liquid, or gaseous fuel, e.g. hypergolic fuel
  • F41A 1/06 Adjusting the range without varying elevation angle or propellant charge data, e.g. by venting a part of the propulsive charge gases, or by adjusting the capacity of the cartridge or combustion chamber